Logbook entries, work orders, 8130-3 tags, ADs and service bulletins, explained with interactive examples from one invented jet and a 12-question quiz.
Israel Slowdowitz11 min read
Updated
An aircraft’s logbooks are its maintenance history, written by the people who did the work. When a jet is bought, financed, leased or inspected, someone reads them to answer a plain question: what was done to this aircraft, when, and who signed for it?
This guide follows one invented midsize jet through its records. It covers what sits on the records shelf, how to read a single entry, how work orders and 8130-3 tags back that entry up, and how Airworthiness Directives differ from service bulletins. Most figures are interactive, and a 12-question quiz at the end checks what stuck.
What the FAA requires you to keep
The owner’s recordkeeping rule, 14 CFR 91.417, splits an aircraft’s records into two groups.
The first group is the record of each job: a description of the work, the date it was finished, and the signature and certificate number of the person who approved it. The rule lets an owner discard these once the work is repeated or superseded, or a year after it was done.
The second group is status: total time on the airframe and on each engine and propeller, the status of life-limited parts, time since overhaul, current inspection status, the list of applicable ADs with how each was complied with, and the forms for major alterations. These records transfer with the aircraft when it is sold.
In practice, owners keep everything. Buyers, appraisers and lenders expect the full history back to the aircraft’s manufacture, and a gap in the records costs money at sale. Back-to-birth records covers where that expectation comes from and how to handle gaps.
One more rule shapes every page. Under 14 CFR 91.407, an aircraft that has had maintenance cannot fly until an authorized person approves it for return to service and the logbook entry has been made. Writing the entry is part of finishing the job.
What’s in a set of aircraft records
The records for a small piston airplane can fit in three thin books: airframe, engine and propeller. A business jet’s records fill a shelf, and they are organized around one idea: records follow serial numbers.
Engines, the APU and many components come off the aircraft for overhaul or exchange and end up on other aircraft. Each keeps its own logbook or history card, and the record moves with the part. The airframe logbook records only the removal and the installation.
Stays with the aircraftS/NFollows a serial number
Airframe logbook
Stays with the aircraft for its whole life.
HoldsInspections, repairs, alterations, AD compliance, and every part installed on or removed from the airframe. An engine change shows up here as one removal and one installation.
Check firstEntries in date order, total time that only goes up, and a signed return to service after every inspection.
Engine logbook, left
Follows engine S/N E-10388 wherever it goes.
HoldsEngine hours and cycles, borescope and hot section inspections, module changes, overhauls, and engine ADs and service bulletins.
Check firstHours and cycles that carry forward from entry to entry, and the cycles left on every life-limited part.
Engine logbook, right
Follows engine S/N E-10412 wherever it goes.
HoldsThe same kinds of entries as the left engine, for a different engine. The two rarely show the same hours, because engines are swapped and overhauled on their own schedules.
Check firstHours and cycles that carry forward from entry to entry, and the cycles left on every life-limited part.
APU logbook
Follows APU S/N P-2231.
HoldsAPU hours and starts, inspections, repairs and overhauls. The APU mostly runs on the ground, so it keeps its own hour meter, separate from aircraft time.
Check firstAPU hours that match the status report, and a history for every APU serial number the aircraft has carried.
Status records
Must transfer with the aircraft when it is sold.
HoldsTotal time on the airframe and each engine, inspection status, life-limited parts, time since overhaul, and the AD list with how each AD was complied with. Most operators print these from a maintenance tracking system.
Check firstEvery line should trace back to a signed entry. A status report is only as good as the entries behind it.
Component records
Each card follows one serialized part.
HoldsInstallation and removal history for landing gear, starters, actuators, fire bottles and other tracked parts, with hours, cycles and shop visits for each.
Check firstAn unbroken history for every life-limited part. A gap in the cycles is a question for the seller.
Work order packages
One package per shop visit.
HoldsThe shop’s job file for each visit: task cards, findings, parts records and inspection sign-offs. The logbook entry is the summary of it.
Check firstWhen an entry says “see work order,” the package is part of the record. It belongs with the logbooks.
Release certificates
Each certificate names specific part and serial numbers.
HoldsFAA Form 8130-3 tags for new and overhauled parts, EASA Form 1s, and other release paperwork that came with installed parts.
Check firstThe serial number on each tag matches the part and the entry that installed it.
Alterations
Stays with the aircraft.
HoldsForm 337s for major repairs and alterations, supplemental type certificates, flight manual supplements, and weight and balance revisions.
Check firstApproval paperwork for every modification on the aircraft. A modification with no 337 or STC behind it is a finding.
Engine logbook, right (exchange engine)
Arrived with engine S/N E-11077.
HoldsIts own history from other aircraft: 6,210.4 hours and 5,102 cycles since new. That is more time than the airframe it now sits on, and both numbers are correct.
Check firstA complete history back to new, including the years it flew for other operators, before anyone relies on its times.
Airframe logbook
Stays with the aircraft for its whole life.
Latest entryRemoved right engine S/N E-10412. Installed right engine S/N E-11077 IAW the maintenance manual. Ops check good.
What movedEngine E-10412 left with its own logbook. The airframe log keeps this one entry about the swap, and the engine records hold everything else.
or tap any book
Figure 1The records set for an invented midsize jet. Engines, the APU, components and tags follow their serial numbers, so their records can leave the aircraft.
Two things follow for anyone reviewing a set. The aircraft’s total time and an engine’s total time are often different numbers, and both can be right. And a component’s history can begin years before it was installed on this aircraft, so part of its record may come from other operators.
How to read a logbook entry
Many entries today, especially from repair stations, are printed on a sticker, pasted into the logbook and signed. Older entries are handwritten. The required content is the same.
For maintenance, 14 CFR 43.9 requires four things: a description of the work or a reference to data that describes it, the date the work was completed, the name of the person who did it if someone else approved it, and the approver’s signature, certificate number and kind of certificate. Inspection entries follow 14 CFR 43.11, which adds the type and extent of the inspection, the aircraft’s total time, and a return-to-service statement. The signature approves return to service only for the work described in that entry.
Step through the entry below. Each highlight is one thing a reviewer looks for.
3.C/W AD 2026-05-12 BY INSPECTION OF MAIN WHEEL TIE BOLTSIAW SB 32-0091 REV 1. NO DEFECTS.RECURRING, NEXT DUE 4,712.3 HRS.
PHASE 3 INSPECTION PERFORMED IAW THE INSPECTIONS AND PROCEDURES OF THE MFR INSPECTION PROGRAM. AIRCRAFT FOUND AIRWORTHY AND APPROVED FOR RETURN TO SERVICE.
M. OKAFOR, INSPECTOR
1Date
The date the work was finished. Every maintenance entry needs one.
14 CFR 43.9(a)(2)
2Aircraft times
Total time in service and landings when the work was done. Inspection entries must show total time, and every future due date is counted from these numbers.
14 CFR 43.11(a)(2)
3Work order
The shop’s job number for this visit. The task cards, findings and parts paperwork behind this entry are filed under it.
FAA AC 43-9D, para. 8.4
4What was done
One numbered item per job, in plain words: inspected, removed, installed, checked. The rule also allows a reference to data that describes the work instead of a full description.
14 CFR 43.9(a)(1)
5The data it followed
“IAW” names the program, manual section or bulletin the work followed, with its revision. That is how a reviewer checks the work was done to an accepted standard.
14 CFR 43.13(a)
6Parts off and on
Part and serial numbers for what came off and what went on, plus the tracking number from the new wheel’s 8130-3. This line ties the tag to this aircraft.
Compare with block 10 of the tag in figure 5
7AD compliance
The AD number, how it was complied with, and when it comes due again. The AD status record needs all three for a recurring AD.
14 CFR 91.417(a)(2)(v)
8Return to service
The inspection statement, the signature and the certificate it is signed under, here the repair station’s. The signature approves only the work in this entry, and the aircraft cannot fly until it is there.
Wheel assembly replaced · off S/N B1147 · on S/N B2210 · release 8130-3 26-44120 · AMM 32-40-00
Task 3
AD 2026-05-12 · inspection per SB 32-0091 Rev 1 · recurring · next due 4,712.3 hours
Approved by
M. Okafor, inspector · Example Jet Center · repair station X2JR511K
Radar reads each entry into fields like these and keeps a link back to the page it came from, so every line on a due list can be checked against a signed record.
Figure 2One entry from the airframe logbook, taken apart. The shop, people and numbers are invented.
Entries lean on shorthand. These are the abbreviations you will see most:
Shorthand
Meaning
C/W
Complied with
IAW
In accordance with, followed by the data the work used
Illustrated parts catalog, used to confirm part numbers
NRC
Non-routine card: a finding written up during a job
Ops check
Operational check after an installation
A&P, IA
Airframe and powerplant mechanic; inspection authorization, which an A&P needs to sign an annual inspection
Numbers like 32-40-00 come from the ATA chapter system that most manuals share. Chapter 32 is landing gear, 49 is the APU, chapters 71 through 80 cover the engine, and 05 holds time limits and inspection programs. Once you know a few chapters, you can scan a page of entries and see which systems were worked on.
Hours, cycles and the calendar
Entries record the aircraft’s clocks at the time of the work. There are three, and different items run on each.
Time in service runs from the moment the aircraft leaves the ground until it touches down at the next landing (14 CFR 1.1). It is shorter than the flight time in a pilot’s logbook, which also counts taxi.
Cycles count landings for the airframe. Engines count cycles as their manufacturer defines them, usually one per flight. Each flight pressurizes the fuselage once, and each start and shutdown heats and spins up the disks inside a turbine engine, so most of their limits are written in cycles.
The calendar covers what ages on the ground: inspections due every so many months, transponder and altimeter checks every 24 calendar months, and parts with shelf lives.
Many limits use two clocks at once: 300 hours or 12 months, whichever comes first. Fly the example aircraft forward and watch the order in which items come due.
Time in service
4,512.3
hours
Cycles
3,874
landings
Calendar
12 Sep 2026
today
A trip is three legs: 5.8 hours, 3 landings, 4 days. A month is 32.5 hours and 18 landings.
AD 2026-05-12 tie bolt inspection
OK
Every 200 hours. Last done at 4,512.3 hours.
Hours
200.0 hours left
Next scheduled inspection
OK
Every 300 hours or 12 months, whichever comes first.
Hours
Months
300.0 hours left
Transponder test
OK
Every 24 calendar months (14 CFR 91.413). Tested 18 Jan 2025, so good through 31 Jan 2027.
Calendar
5 months left
Main landing gear life limit
OK
20,000 landings. Installed new when the aircraft was built.
Landings
16,126 landings left
Figure 3One aircraft, three clocks. The transponder interval comes from 14 CFR 91.413; the other limits are invented for the example.
Work orders: the detail behind the entry
When an aircraft goes into a shop, the shop opens a work order: a numbered job file for that visit. The requested work becomes task cards, which technicians sign as they finish each step and inspectors sign again where the shop requires a second check. Anything found along the way gets a non-routine card with the finding and the fix. Parts arrive from stores with their release paperwork.
At the end, the shop writes the logbook entry. A phase inspection can produce a work order hundreds of pages long and a logbook entry of a dozen lines, so the entry refers to the work order instead of repeating it.
That reference matters. Section 43.9 lets an entry describe the work by referring to other data, and the FAA’s records guidance, AC 43-9D, says referenced documents such as work orders are to be made part of the maintenance records and kept. The shop has to keep its own copy for only two years, and it must give the owner a copy of the maintenance release (14 CFR 145.219). After those two years, the owner’s copy of the work order may be the only one left. Keep work order packages with the logbooks.
WO 26-0917 · 214 pages
Crew discrepancy log06 SEP 2026
Vibration felt from the left main gear during taxi. Worse in turns.
Reported by: captain→ WO 26-0917, item 3
Work order 26-0917Example Jet Center
Opened 08 SEP 2026
Item 1Phase 3 inspection
Item 2AD 2026-05-12 per SB 32-0091 Rev 1
Item 3Crew squawk: LH main gear vibration
Task card 32-10WO 26-0917
Inspect main wheels, brakes and bearings IAW AMM 32-40-00
✓ Remove main wheelsJA
✓ Inspect bearings and racesJA
✓ Inspector buy-backMO
Non-routine card 4WO 26-0917
FoundLH main wheel inner bearing race pitted.
ActionReplaced wheel assembly IAW AMM 32-40-00.
Tech JAInsp MO
Parts issueWO 26-0917
PartWheel assy P/N 5009134-3, qty 1
SerialB2210, overhauled
ReleaseFAA 8130-3, tracking 26-44120
8130-3
Close-outWO 26-0917
✓ Final inspection completeMO
✓ Logbook entry made12 SEP 2026
✓ Copy of package to owner
Airframe logbook
WORK ORDER 26-0917 · 12 SEP 2026
1. PERFORMED PHASE 3 INSPECTION…
1. Squawk The crew writes up a problem. It becomes an item on the work order.
2. Work order The shop opens a numbered job file for the visit and lists the requested work.
3. Task card Each job gets a card. Technicians sign each step, and an inspector signs where the shop requires a second check.
4. Finding Anything found along the way gets its own non-routine card: what was found and what was done about it.
5. Parts Parts come from stores with their release paperwork. The wheel’s 8130-3 goes into the package.
6. Close-out After the final inspection, the shop writes the logbook entry and gives the owner a copy of the package. The entry points back to the work order by number.
Figure 4The paperwork behind the entry in figure 2. A real phase inspection package runs to hundreds of pages; this shows one of each kind.
8130-3 tags: release paperwork for parts
Parts travel with paperwork too. In the US the best-known piece is FAA Form 8130-3, the Authorized Release Certificate, which the industry calls an 8130 or a tag. It certifies one of two things about the parts listed on it.
A manufacturer uses block 13 to certify that a new part conforms to its approved design and is in a condition for safe operation. A repair station uses block 14 to certify that it did the work described on the form under Part 43 and approves the part for return to service. Only one side is filled in, and the other is shaded out. Block 11 tells you which case you are looking at: NEW for a new part, or OVERHAULED, REPAIRED, INSPECTED, TESTED or MODIFIED for a part that has been through a shop, with block 12 describing the work and the standard used.
Europe’s equivalent is the EASA Form 1. A shop approved by both the FAA and EASA can issue a dual release: one 8130-3 that serves as both.
Block 1 · Approving authority Preprinted as FAA/United States on the US form.
Block 2 · Title Authorized Release Certificate, FAA Form 8130-3, Airworthiness Approval Tag. In the hangar it is “an 8130” or “the tag.”
Block 3 · Form tracking number A unique number the issuer gives this certificate. The logbook entry in figure 2 cites it, which ties this tag to that installation.
Block 4 · Organization Who issued the certificate: the manufacturer for a new part, or the repair station that did the work.
Block 5 · Work order, contract or invoice The issuer’s own job or sales number. It leads to the issuer’s records for this part. It is a different number from the aircraft’s work order.
Block 6 · Item The line number. One form can list several parts, and each line needs its own identity.
Block 7 · Description What the part is, in words.
Block 8 · Part number Has to match the part and the parts catalog for the aircraft it goes on, including the dash number.
Block 9 · Quantity How many parts the line covers.
Block 10 · Serial number Ties the certificate to one physical part. It must match the data plate on the part and the entry that installs it.
Block 11 · Status/work What the certificate is for. A manufacturer enters NEW (PROTOTYPE and USED cover special cases). After maintenance, a shop enters OVERHAULED, REPAIRED, INSPECTED, TESTED or MODIFIED, and block 12 has to describe the standard it used.
Block 12 · Remarks The details behind block 11: the work done and the manual it followed, with revision, plus ADs or bulletins complied with and anything else the signer puts on record.
Blocks 13a to 13e · Production release A manufacturer certifies the part was made to its design data and, with the first box checked, is in a condition for safe operation. This side is shaded out when the form is a maintenance release.
Blocks 14a to 14e · Maintenance release The shop certifies that the work in blocks 11 and 12 was done under 14 CFR Part 43 and approves the part for return to service. This side is shaded out on a new-part release.
Match it: the wheel, its tag and the entry have to agree
All three agree, so the tag documents this wheel.The wheel says B2201 and the tag says B2210. The tag documents a different wheel, so this one waits until the shop that issued the tag sorts it out. Nobody corrects a tag by hand.
Figure 5FAA Form 8130-3, block by block, for the wheel installed in figure 2. Tap any block. Companies, people and numbers are invented.
The form has three limits:
The form does not authorize installing the part on a particular aircraft. The form says so itself, and the installer still checks that the part is eligible for the aircraft’s configuration.
It is not the only acceptable release. The FAA’s parts guidance, AC 20-62E, also accepts a repair station tag, a work order or a maintenance record entry that carries the required information.
A tag covers one shop visit. For a life-limited part you need its full history of cycles back to new, and the latest tag says nothing about earlier visits.
Service bulletins come from manufacturers. An airframe, engine or component maker publishes one when it wants operators to inspect, modify or replace something. For an aircraft operated under Part 91, the FAA treats a service bulletin as advisory: compliance is not required unless an Airworthiness Directive includes it. That holds even when the manufacturer prints MANDATORY across the top. The label tells you how seriously the manufacturer takes the problem.
Airworthiness Directives come from the FAA. Part 39 calls them legally enforceable rules, and operating a product that does not meet an applicable AD is a violation. An AD applies to every product in its applicability statement, including one that has been modified in the affected area.
The two often travel together. When the FAA decides that a problem a manufacturer has found is an unsafe condition, it can write an AD that requires the actions in the service bulletin. The bulletin then becomes part of the AD, and where the two disagree, the AD controls (14 CFR 39.27). Most ADs start as a proposed rule open for public comment. Urgent ones are issued as final rules without prior notice, and emergency ADs are sent straight to registered owners.
Manufacturer
Example Aircraft Co.Mandatory
Service Bulletin 32-0091, Rev 1
SubjectMain wheel tie bolt inspection
ActionInspect tie bolts for cracks at each tire change.
Required by AD 2026-05-12
Advisory under Part 91
Required, through the AD
incorporated by reference
FAA
14 CFR Part 39Proposed rule
Proposed AD: Example Aircraft Co. airplanes
The FAA proposes to require the inspection in SB 32-0091 Rev 1.
Comments open to the public before the rule becomes final.
14 CFR Part 39Final rule
AD 2026-05-12
Applies toExample Aircraft Co. model EX-500, serial numbers 0001 to 0450
RequiredWithin 100 hours, inspect the main wheel tie bolts IAW SB 32-0091 Rev 1. Repeat every 200 hours.
1. The manufacturer publishes a service bulletin Example Aircraft Co. finds cracked wheel tie bolts and publishes SB 32-0091. It prints MANDATORY on the cover. For an aircraft operated under Part 91, the bulletin is still advisory.
2. The FAA proposes an AD The FAA decides the cracks are an unsafe condition and publishes a proposed rule. Anyone can comment before it becomes final.
3. The final AD requires the bulletin’s inspection The bulletin is now part of the AD, and where the two differ, the AD controls. Doing the inspection any other way takes an approved alternative method of compliance.
4. The owner records compliance Each inspection updates the AD status record: AD number, revision, method of compliance and next due. That record transfers with the aircraft.
Figure 6How a service bulletin becomes mandatory. The manufacturer, model and documents are invented.
Service bulletin
Airworthiness Directive
Issued by
The manufacturer
The FAA
Under Part 91
Advisory, unless an AD requires it
Mandatory for every product it lists
Numbering
The manufacturer’s own, often by ATA chapter: SB 32-0091
Year, biweekly period, sequence: AD 2026-05-12
Compliance record
An entry citing the bulletin and its revision
AD number, revision date, method of compliance, and next due if it recurs
Doing it another way
No approval needed, since it is advisory
Requires an approved alternative method of compliance (AMOC)
Two kinds of requirements apply without any AD. Replacement times and inspections in a manufacturer’s airworthiness limitations section are mandatory (14 CFR 91.403(c)). And a multiengine jet does not get an annual inspection: 14 CFR 91.409(e) requires it to follow an inspection program the operator selects, most often the manufacturer’s, so the tasks in that program become the aircraft’s inspection requirements.
Contracts can add more. An engine maintenance program, a lease or a loan agreement can require specific bulletins, which is one reason buyers ask about service bulletin status even where the law does not.
Required or recommended? Open a card to check.
Service bulletinLabeled MANDATORY by the manufacturer. No AD mentions it. The jet flies under Part 91.Check
RecommendedThe FAA treats a Part 91 service bulletin as advisory unless an AD includes it. An engine program or a lease can still require it by contract.
Bulletin inside an ADThe same bulletin, after the FAA issues an AD that requires its inspection.Check
RequiredThe bulletin is now part of the AD. The AD decides which aircraft, by when, and how (14 CFR 39.27).
Airworthiness limitationA replacement time listed in the airworthiness limitations section of the maintenance manual.Check
Required14 CFR 91.403(c) makes airworthiness limitations mandatory, with or without an AD.
Service letterA manufacturer’s letter recommending a new cleaning product for the windshield.Check
RecommendedService letters share tips and background. On their own, they carry no legal requirement.
Figure 7What makes maintenance required for an aircraft operated under Part 91.
For recurring ADs, check the next-due math yourself. Recurring ADs walks through how.
A first pass through a set of logbooks
When a set of records lands on your desk, work through it in this order:
Read the status records first. Current times, inspection status, the AD list and life-limited parts tell you what the rest of the set has to prove.
Check that time only moves forward. Total time and landings should rise from entry to entry. A drop or a gap needs an explanation.
Follow each big event to its paperwork. For every inspection, engine change and repair, find the entry, the work order and the part tags.
Match serial numbers. The part’s data plate, its tag and the entry that installed it should agree.
Walk the AD list. For each AD, confirm it applies, check the recorded method of compliance, and recompute the next due for anything that recurs.
Find the paperwork behind every modification. Each alteration should have its Form 337 or STC.
Write gaps down as questions. A missing record is a question for the seller or the shop until someone answers it.
Twelve questions, each tied to a section above. Pick an answer to see the explanation.
Question 1 of 12Score 0
Question 1
A shop finishes a brake change Tuesday night and plans to write the logbook entry Thursday. Can the aircraft fly Wednesday?
Show the answer
Answer B: No. It needs an approval for return to service and the entry before it flies.14 CFR 91.407 says an aircraft that has had maintenance cannot be operated until it is approved for return to service and the required record entry has been made.Read: What the FAA requires you to keep
Question 2
Which of these does 14 CFR 43.9 require in every maintenance entry?
Show the answer
Answer B: The date the work was completed43.9 requires a description of the work (or a reference to data that describes it), the completion date, the name of whoever did the work if someone else approved it, and the approver’s signature, certificate number and kind of certificate. Total time is required in inspection entries under 43.11, and most shops record it on every entry anyway.Read: How to read a logbook entry
Question 3
Why does each engine on a jet have its own logbook?
Show the answer
Answer A: Engines come off for overhaul or exchange, and their history has to follow the engine’s serial number.Engines, APUs and many components move between aircraft. A record for each serial number lets the history travel with the part. The airframe logbook records only the removal and the installation.Read: What’s in a set of aircraft records
Question 4
For maintenance records, when does time in service start?
Show the answer
Answer C: When the aircraft leaves the ground14 CFR 1.1 defines time in service as the time from when the aircraft leaves the surface of the earth until it touches down at the next landing.Read: Hours, cycles and the calendar
Question 5
Which clock sets the life limit for most rotating parts inside a turbine engine, such as the disks?
Show the answer
Answer B: CyclesEvery start, takeoff and shutdown loads the disks with heat and spin. Manufacturers publish life limits for these parts in cycles, and the engine records have to account for every cycle since new.Read: Hours, cycles and the calendar
Question 6
When is this AD next due?
AD 2026-05-12 · repeat every 200 hours · last done at 4,512.3 hours
Show the answer
Answer A: 4,712.3 hoursAdd the interval to the aircraft time at the last compliance. The AD status record has to show that next-due point for every recurring AD, and an AD does not wait for a scheduled inspection.Read: Hours, cycles and the calendar
Question 7
An entry ends with “Ref WO 26-0917.” What should happen to work order 26-0917?
Show the answer
Answer B: Keep it with the logbooks. A work order referenced in an entry becomes part of the maintenance record.FAA AC 43-9D says documents referenced in an entry, such as work orders, are to be made part of the maintenance records and kept. The shop only has to keep its own copy for two years.Read: Work orders: the detail behind the entry
Question 8
An 8130-3 arrives with this in block 11. What does it tell you?
Block 11, Status/Work: OVERHAULED
Show the answer
Answer B: A shop overhauled the part and approved it for return to service in block 14.OVERHAULED is a maintenance status, certified in block 14. New parts show NEW and use block 13. Neither side authorizes installing the part on a particular aircraft; the installer checks eligibility.Read: 8130-3 tags: release paperwork for parts
Question 9
A starter-generator arrives with this paperwork. What happens next?
Data plate: S/N 4471 · 8130-3 block 10: S/N 4417
Show the answer
Answer C: Hold the part until the mismatch is resolved.A tag documents one specific part. If the serial numbers disagree, the tag does not document this part, and nobody should alter a tag to make it match.Read: 8130-3 tags: release paperwork for parts
Question 10
A manufacturer prints MANDATORY on a service bulletin. No AD mentions it, and the jet flies under Part 91. Do FAA rules require compliance?
Show the answer
Answer B: No, though a contract or engine program may still require it.The FAA treats service bulletins as advisory for Part 91 operators unless an AD includes them. The label signals the manufacturer’s concern, and contracts or engine programs can still make it required.Read: ADs vs. service bulletins
Question 11
An AD requires the inspection in SB 32-0091. The bulletin allows 150 hours to comply and the AD allows 100. Which applies?
Show the answer
Answer B: 100 hours. Where the two conflict, the AD controls.14 CFR 39.27: a service document incorporated into an AD becomes part of it, and if the two conflict, you follow the AD.Read: ADs vs. service bulletins
Question 12
Which record must transfer with the aircraft when it is sold?
Show the answer
Answer B: The current status of applicable ADs, including the method of compliance14 CFR 91.417 requires the status records to transfer with the aircraft: total times, life-limited part status, time since overhaul, inspection status, AD status and the forms for major alterations.Read: What the FAA requires you to keep