FAA Repairman Certificate – Light-Sport
Aircraft (LSA) Inspection – Airplane Practice
Exam | All Questions And Solutions
(Answers+Rationales) | Exam Prep 2026/2027
1. Which regulatory part of 14 CFR governs the certification requirements for a light-
sport aircraft repairman?
a) 14 CFR Part 43
b) 14 CFR Part 65
c) 14 CFR Part 61
d) 14 CFR Part 91
14 CFR Part 65, Subpart E sets forth the specific eligibility, privileges, and performance
standards required to hold an FAA Repairman Certificate (Light-Sport Aircraft) with an
Inspection or Maintenance rating.
2. An individual holding a Light-Sport Aircraft Repairman Certificate with an
Inspection rating is primary privileged to perform which of the following actions?
a) Annual condition inspections on any experimental or special light-sport aircraft owned
by any party.
b) Annual condition inspections on an experimental light-sport aircraft (ELSA) owned
by the certificate holder.
c) Major repairs and alterations on special light-sport aircraft (SLSA) used for
commercial flight instruction.
d) 100-hour inspections on special light-sport aircraft operating for hire.
The Inspection rating privileges are limited strictly to performing the annual condition
inspection on an experimental light-sport aircraft (ELSA) that is owned by the certificate
holder and registered under 14 CFR 21.191(i).
3. What is the minimum course duration mandated by the FAA for a Light-Sport
Aircraft Repairman Inspection course for airplane class?
, a) 8 hours
b) 16 hours
c) 80 hours
d) 120 hours
An FAA-accepted Light-Sport Aircraft Repairman Inspection course for the airplane class must
consist of a minimum of 16 hours of instruction covering regulatory and technical subjects.
4. Under 14 CFR Part 91, how often must an annual condition inspection be
performed on an Experimental Light-Sport Aircraft (ELSA) to maintain
airworthiness?
a) Every 12 calendar months
b) Every 100 hours of time in service
c) Every 24 calendar months
d) Every 6 calendar months
14 CFR Part 91 operating limitations state that no person may operate an ELSA unless within
the preceding 12 calendar months it has received a condition inspection in accordance with
FAA standards.
5. Where are the operating limitations for an Experimental Light-Sport Aircraft
usually documented?
a) On the aircraft data plate attached to the fuselage.
b) In the manufacturer’s structural repair manual.
c) Attached to FAA Form 8130-7 (Special Airworthiness Certificate).
d) Inside the pilot logbook under endorsement entries.
Operating limitations are issued by the FAA inspector or DAR as part of FAA Form 8130-7
(Special Airworthiness Certificate) and must be displayed or carried in the aircraft during
operation.
6. When performing an annual condition inspection on an airplane LSA, what
primary document must be utilized as the visual baseline for acceptable methods,
techniques, and practices if manufacturer manuals are silent?
, a) FAA-H-8083-30 (Aviation Maintenance Technician Handbook)
b) AC 43.13-1B/2B (Acceptable Methods, Techniques, and Practices - Aircraft
Inspection and Repair)
c) Order 8130.2 (Airworthiness Certification of Aircraft)
d) 14 CFR Part 147 Curriculum Guidelines
AC 43.13-1B/2B serves as the standard reference for acceptable aviation practices, methods,
and structural repairs when specific manufacturer instructions do not prescribe a procedure.
7. A light-sport aircraft inspector discovers a minor structural crack in an ELSA wing
rib. What is the proper procedure before approving the aircraft for return to
service?
a) Submit FAA Form 337 to the local FSDO for prior approval.
b) Repair the crack using standard aircraft maintenance methods (AC 43.13-1B) and
record the maintenance entry in the aircraft logbook.
c) Obtain written manufacturer authorization prior to applying any structural repair patch.
d) Re-evaluate the aircraft through a full flight test phase prior to signing off the
condition inspection.
Experimental Light-Sport Aircraft (ELSA) owners holding an inspection rating may perform
repairs using standard acceptable industry methods (such as AC 43.13-1B) and record the
completion in the aircraft maintenance logbook.
8. What minimum age requirement must an applicant meet to be eligible for a Light-
Sport Aircraft Repairman Certificate?
a) 16 years old
b) 17 years old
c) 18 years old
d) 21 years old
14 CFR 65.107 stipulates that an applicant for an LSA repairman certificate must be at least 18
years of age.
, 9. In which location must the permanent builder/manufacturer data plate be installed
on an LSA airplane?
a) On the instrument panel in full view of the pilot.
b) Externally on the fuselage exterior near the tail or rear entrance door.
c) Inside the engine compartment attached to the firewall.
d) On the main landing gear leg structural support.
14 CFR 45.11 requires fireproof identification plates to be secured on the exterior fuselage,
accessible and legible, typically near the tail surfaces or rear cabin door.
10. What is the maximum takeoff weight (MTOW) limit defined by 14 CFR 1.1 for a
landplane light-sport aircraft?
a) 1,230 pounds
b) 1,320 pounds
c) 1,430 pounds
d) 1,600 pounds
14 CFR 1.1 defines a light-sport landplane as having a maximum takeoff weight of not more
than 1,320 pounds (600 kilograms).
11. During a condition inspection of a composite wing spar, an inspector observes
localized surface delamination. Which non-destructive testing method is most
appropriate for initial field verification?
a) Dye penetrant test
b) Coin-tap testing (auditory resonance)
c) Magnetic particle inspection
d) Eddy current inspection
Coin-tap testing is an effective, non-destructive field inspection technique to detect
subsurface delamination or debonding in light-sport composite structures.
12. What entry must be made in the aircraft maintenance records upon completing a
successful annual condition inspection on an ELSA?
Aircraft (LSA) Inspection – Airplane Practice
Exam | All Questions And Solutions
(Answers+Rationales) | Exam Prep 2026/2027
1. Which regulatory part of 14 CFR governs the certification requirements for a light-
sport aircraft repairman?
a) 14 CFR Part 43
b) 14 CFR Part 65
c) 14 CFR Part 61
d) 14 CFR Part 91
14 CFR Part 65, Subpart E sets forth the specific eligibility, privileges, and performance
standards required to hold an FAA Repairman Certificate (Light-Sport Aircraft) with an
Inspection or Maintenance rating.
2. An individual holding a Light-Sport Aircraft Repairman Certificate with an
Inspection rating is primary privileged to perform which of the following actions?
a) Annual condition inspections on any experimental or special light-sport aircraft owned
by any party.
b) Annual condition inspections on an experimental light-sport aircraft (ELSA) owned
by the certificate holder.
c) Major repairs and alterations on special light-sport aircraft (SLSA) used for
commercial flight instruction.
d) 100-hour inspections on special light-sport aircraft operating for hire.
The Inspection rating privileges are limited strictly to performing the annual condition
inspection on an experimental light-sport aircraft (ELSA) that is owned by the certificate
holder and registered under 14 CFR 21.191(i).
3. What is the minimum course duration mandated by the FAA for a Light-Sport
Aircraft Repairman Inspection course for airplane class?
, a) 8 hours
b) 16 hours
c) 80 hours
d) 120 hours
An FAA-accepted Light-Sport Aircraft Repairman Inspection course for the airplane class must
consist of a minimum of 16 hours of instruction covering regulatory and technical subjects.
4. Under 14 CFR Part 91, how often must an annual condition inspection be
performed on an Experimental Light-Sport Aircraft (ELSA) to maintain
airworthiness?
a) Every 12 calendar months
b) Every 100 hours of time in service
c) Every 24 calendar months
d) Every 6 calendar months
14 CFR Part 91 operating limitations state that no person may operate an ELSA unless within
the preceding 12 calendar months it has received a condition inspection in accordance with
FAA standards.
5. Where are the operating limitations for an Experimental Light-Sport Aircraft
usually documented?
a) On the aircraft data plate attached to the fuselage.
b) In the manufacturer’s structural repair manual.
c) Attached to FAA Form 8130-7 (Special Airworthiness Certificate).
d) Inside the pilot logbook under endorsement entries.
Operating limitations are issued by the FAA inspector or DAR as part of FAA Form 8130-7
(Special Airworthiness Certificate) and must be displayed or carried in the aircraft during
operation.
6. When performing an annual condition inspection on an airplane LSA, what
primary document must be utilized as the visual baseline for acceptable methods,
techniques, and practices if manufacturer manuals are silent?
, a) FAA-H-8083-30 (Aviation Maintenance Technician Handbook)
b) AC 43.13-1B/2B (Acceptable Methods, Techniques, and Practices - Aircraft
Inspection and Repair)
c) Order 8130.2 (Airworthiness Certification of Aircraft)
d) 14 CFR Part 147 Curriculum Guidelines
AC 43.13-1B/2B serves as the standard reference for acceptable aviation practices, methods,
and structural repairs when specific manufacturer instructions do not prescribe a procedure.
7. A light-sport aircraft inspector discovers a minor structural crack in an ELSA wing
rib. What is the proper procedure before approving the aircraft for return to
service?
a) Submit FAA Form 337 to the local FSDO for prior approval.
b) Repair the crack using standard aircraft maintenance methods (AC 43.13-1B) and
record the maintenance entry in the aircraft logbook.
c) Obtain written manufacturer authorization prior to applying any structural repair patch.
d) Re-evaluate the aircraft through a full flight test phase prior to signing off the
condition inspection.
Experimental Light-Sport Aircraft (ELSA) owners holding an inspection rating may perform
repairs using standard acceptable industry methods (such as AC 43.13-1B) and record the
completion in the aircraft maintenance logbook.
8. What minimum age requirement must an applicant meet to be eligible for a Light-
Sport Aircraft Repairman Certificate?
a) 16 years old
b) 17 years old
c) 18 years old
d) 21 years old
14 CFR 65.107 stipulates that an applicant for an LSA repairman certificate must be at least 18
years of age.
, 9. In which location must the permanent builder/manufacturer data plate be installed
on an LSA airplane?
a) On the instrument panel in full view of the pilot.
b) Externally on the fuselage exterior near the tail or rear entrance door.
c) Inside the engine compartment attached to the firewall.
d) On the main landing gear leg structural support.
14 CFR 45.11 requires fireproof identification plates to be secured on the exterior fuselage,
accessible and legible, typically near the tail surfaces or rear cabin door.
10. What is the maximum takeoff weight (MTOW) limit defined by 14 CFR 1.1 for a
landplane light-sport aircraft?
a) 1,230 pounds
b) 1,320 pounds
c) 1,430 pounds
d) 1,600 pounds
14 CFR 1.1 defines a light-sport landplane as having a maximum takeoff weight of not more
than 1,320 pounds (600 kilograms).
11. During a condition inspection of a composite wing spar, an inspector observes
localized surface delamination. Which non-destructive testing method is most
appropriate for initial field verification?
a) Dye penetrant test
b) Coin-tap testing (auditory resonance)
c) Magnetic particle inspection
d) Eddy current inspection
Coin-tap testing is an effective, non-destructive field inspection technique to detect
subsurface delamination or debonding in light-sport composite structures.
12. What entry must be made in the aircraft maintenance records upon completing a
successful annual condition inspection on an ELSA?
