# N286F: 1960 Lockheed 188C

- Status: Valid registration
- Airframe: [Lockheed 188C](https://openairdocs.org/model/lockheed-188c) (registry code 5262604, 102 seats)
- Engine: [Allison 501-D13 series](https://openairdocs.org/engine/allison-501-d13-series) (registry code 03004)
- Data sheets: [TCDS 4A22](https://openairdocs.org/tcds/4A22) (Lockheed Martin Corporation), [TCDS E-282](https://openairdocs.org/tcds/E-282) (Rolls-Royce Corporation) (OpenAirDocs)
- Serial number: 1146
- Year built: 1960
- Type: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: January 11, 1961
- Certificate issued: September 29, 2009
- Expires: September 30, 2028
- Mode S code: A2E4C2
- Registered owner: [Rockland Aerospace Inc](https://openairdocs.org/faa-owner/ROCKLAND%20AEROSPACE%20INC)
- Location: [Crofton, MD](https://openairdocs.org/faa-place/MD/Crofton)
- Owner type: Corporation
- Owner's area on the map: 39.0097° N, 76.6839° W: Placed by OpenAirDocs at the center of ZIP code 21114, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=286F
- Page: https://openairdocs.org/aircraft/N286F

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Allison 501-D13 model are included.

## ADs that may apply (OpenAirDocs): 77 in force

### Matched by airframe (Lockheed 188C)

- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2018-11-02](https://openairdocs.org/ad/2018-11-02): Flight Controls · Lockheed Martin 188A, 188C, P3A and 2 more. Effective May 23, 2018
- [AD 2015-22-07](https://openairdocs.org/ad/2015-22-07): Fuselage · Lockheed Martin 188A and 188C. Effective Dec 10, 2015
- [AD 2015-20-01](https://openairdocs.org/ad/2015-20-01): Wings · Lockheed Martin 188A and 188C. Effective Nov 13, 2015
- [AD 2015-20-05](https://openairdocs.org/ad/2015-20-05): Wings · Lockheed Martin 188A and 188C. Effective Nov 6, 2015
- [AD 2004-22-01](https://openairdocs.org/ad/2004-22-01): Cargo restraint strap assemblies · Cargo restraint straps (Airline Container Manufacturing STC ST01004NY). Effective Dec 1, 2004
- [AD 2000-23-10](https://openairdocs.org/ad/2000-23-10): Donning Oxygen Masks · Lockheed Martin 188A and 188C. Effective Dec 27, 2000
- [AD 99-23-22 R2](https://openairdocs.org/ad/99-23-22-R2): Transponders · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 74 more. Effective Apr 20, 2000
- [AD 98-24-25](https://openairdocs.org/ad/98-24-25): AFM - Limitations Section - Icing · Lockheed Martin 188A and 188C. Effective Dec 30, 1998
- [AD 97-20-02](https://openairdocs.org/ad/97-20-02): AFM - Limitations Section - Power Levers · Lockheed Martin 188A and 188C. Effective Oct 27, 1997
- [AD 89-14-03](https://openairdocs.org/ad/89-14-03): Flap Universal Joints · Lockheed Martin 188A and 188C. Effective Jul 24, 1989
- [AD 87-16-05](https://openairdocs.org/ad/87-16-05): Supplemental Inspections · Lockheed Martin 188A and 188C. Effective Aug 31, 1987
- [AD 87-08-03](https://openairdocs.org/ad/87-08-03): Air Start Door · Lockheed Martin 188A and 188C. Effective May 5, 1987
- [AD 81-03-53 R1](https://openairdocs.org/ad/81-03-53-R1): Fuel Leakage · Lockheed Martin 188A and 188C. Effective Feb 2, 1982
- [AD 81-24-09](https://openairdocs.org/ad/81-24-09): Propeller Performance · Lockheed Martin 188A and 188C. Effective Dec 28, 1981
- [AD 80-10-05](https://openairdocs.org/ad/80-10-05): Wing Front Spar Caps · Lockheed Martin 188A and 188C. Effective Jun 23, 1980
- [AD 80-12-01](https://openairdocs.org/ad/80-12-01): Cargo Door Modifications · Lockheed Martin 188A and 188C with STC SA1754WE or SA2536WE. Effective Jun 9, 1980
- [AD 77-21-09](https://openairdocs.org/ad/77-21-09): Aileron Rudder Balance Interconnect Mechanism · Lockheed Martin 188A and 188C. Effective Nov 25, 1977
- [AD 76-05-02](https://openairdocs.org/ad/76-05-02): Side-Facing Seats · Boeing 707-300B Series, 727-100 Series, 188A and 1 more. Effective Apr 1, 1976
- [AD 74-25-04](https://openairdocs.org/ad/74-25-04): Horizontal Stabilizer · Lockheed Martin 188A and 188C. Effective Jan 3, 1975
- [AD 74-17-01](https://openairdocs.org/ad/74-17-01): Regulator · Boeing 707-100 Long Body, 707-100B Long Body, 707-100B Short Body and 78 more. Effective Sep 16, 1974
- [AD 69-26-08](https://openairdocs.org/ad/69-26-08): Takeoff Warning System · Lockheed Martin 188A and 188C. Effective Jan 10, 1970
- [AD 69-08-07](https://openairdocs.org/ad/69-08-07): Lower Wing Surface · Lockheed Martin 188A and 188C. Effective Apr 17, 1969
- [AD 68-11-02](https://openairdocs.org/ad/68-11-02): Upper & Lower Wing Planks · Lockheed Martin 188A and 188C. Effective Jan 4, 1969
- [AD 68-23-05](https://openairdocs.org/ad/68-23-05): Upper Wing Plank · Lockheed Martin 188A and 188C. Effective Dec 6, 1968
- [AD 67-11-04](https://openairdocs.org/ad/67-11-04): Fuselage Main Frames Forging · Lockheed Martin 188A and 188C. Effective Jun 9, 1967
- [AD 66-04-02](https://openairdocs.org/ad/66-04-02): Wing Plank Splice Areas · Lockheed Martin 188A and 188C. Effective Feb 18, 1967
- [AD 67-03-06](https://openairdocs.org/ad/67-03-06): Landing Gear Door Cylinders · Lockheed Martin 188A and 188C. Effective Jan 20, 1967
- [AD 66-28-04](https://openairdocs.org/ad/66-28-04): Nose Landing Gear Steering Housing · Lockheed Martin 188A and 188C. Effective Nov 25, 1966
- [AD 66-11-02](https://openairdocs.org/ad/66-11-02): Lower Wing Plank Splice Areas · Lockheed Martin 188A and 188C. Effective Sep 23, 1966
- [AD 66-05-03](https://openairdocs.org/ad/66-05-03): Outer Wing Cap Fittings · Lockheed Martin 188A and 188C. Effective Feb 19, 1966
- [AD 65-15-04](https://openairdocs.org/ad/65-15-04): No. 4 Wing Plank Drain Holes · Lockheed Martin 188A and 188C. Effective Dec 9, 1965
- [AD 65-21-05](https://openairdocs.org/ad/65-21-05): Vertical Stabilizer Attach Channel · Lockheed Martin 188A and 188C. Effective Oct 11, 1965
- [AD 64-12-05](https://openairdocs.org/ad/64-12-05): Landing Gear Cam Follower · Lockheed Martin 188A and 188C. Effective Sep 28, 1965
- [AD 65-16-01](https://openairdocs.org/ad/65-16-01): Nose Landing Gear Support Link · Lockheed Martin 188A and 188C. Effective Jul 30, 1965
- [AD 65-09-04](https://openairdocs.org/ad/65-09-04): Upper Wing Planks · Lockheed Martin 188A and 188C. Effective Apr 28, 1965
- [AD 64-16-04](https://openairdocs.org/ad/64-16-04): Aileron Push-Pull Tubes · Lockheed Martin 188A and 188C. Effective Mar 2, 1965
- [AD 64-14-05](https://openairdocs.org/ad/64-14-05): Main Landing Gear Support Fitting · Lockheed Martin 188A and 188C. Effective Jun 26, 1964
- [AD 64-11-03](https://openairdocs.org/ad/64-11-03): Upper Wing Planks · Lockheed Martin 188A and 188C. Effective Jun 15, 1964
- [AD 63-17-03](https://openairdocs.org/ad/63-17-03): Horizontal Stabilizer Spar Web · Lockheed Martin 188A and 188C. Effective Nov 21, 1963
- [AD 63-18-03](https://openairdocs.org/ad/63-18-03): Fuselage Stringers · Lockheed Martin 188A and 188C. Effective Sep 17, 1963
- [AD 63-08-03](https://openairdocs.org/ad/63-08-03): Deboost Control System · Lockheed Martin 188A and 188C. Effective May 9, 1963
- [AD 62-26-04](https://openairdocs.org/ad/62-26-04): Elevator Balance Weight Arms · Lockheed Martin 188A and 188C. Effective Dec 4, 1962
- [AD 61-21-05](https://openairdocs.org/ad/61-21-05): Compass Circuit Breakers · Lockheed Martin 188A and 188C. Effective Nov 2, 1961
- [AD 61-15-04](https://openairdocs.org/ad/61-15-04): Safety Belt Grommets · Lockheed Martin 188A and 188C. Effective Aug 2, 1961
- [AD 61-09-01](https://openairdocs.org/ad/61-09-01): Elevator Hydraulic Damper Housing · Lockheed Martin 188A and 188C. Effective Apr 7, 1961
- [AD 60-26-05](https://openairdocs.org/ad/60-26-05): Elevator and Boost Control Valve · Lockheed Martin 188A and 188C. Effective Dec 22, 1960
- [AD 60-26-04](https://openairdocs.org/ad/60-26-04): Swirl Straightener Scoop · Lockheed Martin 188A and 188C. Effective Dec 14, 1960
- [AD 60-24-01](https://openairdocs.org/ad/60-24-01): Fuel Pressure Relief Valve · Lockheed Martin 188A and 188C. Effective Dec 13, 1960

### Matched by engine (Allison 501-D13 series)

- [AD 2006-25-12](https://openairdocs.org/ad/2006-25-12): Removal from service of certain turbine rotor components · Rolls-Royce 501-D13, 501-D13A, 501-D13D and 6 more. Effective Jan 23, 2007
- [AD 86-17-06](https://openairdocs.org/ad/86-17-06): Thrust Sensitive Switch Assembly · Rolls-Royce 501-D13, 501-D13A, 501-D13D and 1 more. Effective Sep 15, 1986
- [AD 81-03-02](https://openairdocs.org/ad/81-03-02): 1st Stage Turbine Wheel · Rolls-Royce 501-D13, 501-D13A, 501-D13D and 2 more. Effective Jan 28, 1981
- [AD 80-14-13](https://openairdocs.org/ad/80-14-13): 1st Stage Turbine Wheels · Rolls-Royce 501-D13, 501-D13A, 501-D13D and 2 more. Effective Jul 10, 1980
- [AD 79-25-03](https://openairdocs.org/ad/79-25-03): Second, Third, And Fourth Stage Turbine Wheels · Rolls-Royce 501-D13, 501-D13A, 501-D13D and 2 more. Effective Dec 13, 1979
- [AD 78-09-09](https://openairdocs.org/ad/78-09-09): Third Or Fourth Stage Turbine Wheel · Rolls-Royce 501-D13, 501-D13A, 501-D13D and 2 more. Effective May 12, 1978
- [AD 75-22-05](https://openairdocs.org/ad/75-22-05): Second Stage Turbine Wheels · Rolls-Royce 501-D13, 501-D13A, 501-D13D and 2 more. Effective Oct 23, 1975
- [AD 75-17-32](https://openairdocs.org/ad/75-17-32): Second Stage Turbine Wheels · Rolls-Royce 501-D13, 501-D13A, 501-D13D and 2 more. Effective Aug 14, 1975
- [AD 69-21-03](https://openairdocs.org/ad/69-21-03): First Stage Compressor Wheels · Rolls-Royce 501-D13, 501-D13A, 501-D13D and 6 more. Effective Oct 21, 1969
- [AD 60-21-01](https://openairdocs.org/ad/60-21-01): Torquemeter Housing · Rolls-Royce 501-D13, 501-D13A, 501-D13D and 2 more. Effective Nov 9, 1960
- [AD 60-07-01](https://openairdocs.org/ad/60-07-01): Low Speed Ground Idle · Rolls-Royce 501-D13D and 501-D13E
- [AD 59-21-03](https://openairdocs.org/ad/59-21-03): Compressor Blade · Rolls-Royce 501-D13 and 501-D13A
- [AD 59-18-01](https://openairdocs.org/ad/59-18-01): Low Speed Ground Idle · Rolls-Royce 501-D13 and 501-D13A
- [AD 59-13-01](https://openairdocs.org/ad/59-13-01): Propeller Shaft Roller Bearing · Rolls-Royce 501-D13 and 501-D13A

### Historical (superseded or no longer in force)

- [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996
- [AD 2003-07-02](https://openairdocs.org/ad/2003-07-02) (historical): Turbine rotor components · 501-D13, 501-D13A, 501-D13D and 6 more. Effective May 7, 2003

All 79: https://openairdocs.org/aircraft/N286F/ads.md

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N286F.

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20040511021939I](https://openairdocs.org/incident/20040511021939I), May 11, 2004: Lkheed 188C (N286F), Detroit, MI, Minor damage. (-23) Crew was engaged in a part 91 training flight. Crew made a two-engine out (simulated) landing. #3 & 4 main tires blew during roll-out. Aircraft veered to…

## Service difficulty reports (41)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR ZIAA04059](https://openairdocs.org/sdr/ZIAA04059), Dec 8, 2003: FLOOR SUPPORT. CORRODED. YIP - FOUND RIGHT WING CENTER SECTION RBL 40 AT NR 1 PLANK UPPER SURFACE CORROSION AT FLOOR SUPPORT BRACKET. REMOVED CORROSION AND TREATED AREA PER L-188 SRM 51
- [SDR ZIAA04058](https://openairdocs.org/sdr/ZIAA04058), Sep 20, 2002: DOOR FRAME. CRACKED. YIP - INVESTIGATE X-RAY INDICATIONS AT 2 RIVETS MARKED IN RED ON OUTER SURFACE OF AFT LOWER CARGO DOOR, LOWER FORWARD CORNER. REMOVED REPAIR DOUBLERS TO INVESTI
- [SDR ZIAA04057](https://openairdocs.org/sdr/ZIAA04057), Nov 27, 2001: SKIN. CORRODED. YIP - REMOVE REPAIR INSTALLATION AT RT WING UPPER SURFACE, WS 70, 7/8 PLANK SEAM FOR CO CONVENIENCE. CONFIRM THE EXTENT OF DAMAGE AT THIS LOCATION. INSTALL REPA
- [SDR ZIAA04050](https://openairdocs.org/sdr/ZIAA04050), Sep 6, 2001: FRAME. CRACKED. FOUND FUSELAGE FRAME CRACKED AT FS 716 AT STRINGER 72. REPAIRED FRAME AT STRINGER 68-1 PER L-188 SRM 53-2-3, FIG 2. (M)
- [SDR ZIAA04049](https://openairdocs.org/sdr/ZIAA04049), Sep 6, 2001: FRAME. CRACKED. YIP - FOUND FUSELAGE FRAME CRACKED AT FS 654 BETWEEN STRINGER 9-10. REPAIRED FRAME AT STRINGER 9-10 IAW L-188 SRM 53-2-3, FIG 2. (M)
- [SDR ZIAA04056](https://openairdocs.org/sdr/ZIAA04056), Sep 6, 2001: FRAME. CRACKED. FOUND FUSELAGE FRAME CRACKED AT FS 654 STRINGER 13. REPAIRED FRAME AT STRINGER 13 PER L-188 SRM 53-2-3, FIG 2. (M)
- [SDR ZIAA04043](https://openairdocs.org/sdr/ZIAA04043), Sep 6, 2001: FLOORBEAM. CORRODED. YIP - FOUND FLOORBEAM AT FS 200 RIGHT SIDE NEAR PORTA POTTY AREA CORRODED. REMVOED CORRODED SECTION OF FLOORBEAM AND REPAIRED FS 200 FLOORBEAM PER L-188 SRM 53-
- [SDR ZIAA04055](https://openairdocs.org/sdr/ZIAA04055), Sep 6, 2001: FRAME. CRACKED. FOUND FUSELAGE FRAME CRACKED AT FS 397.5, STRINGER 21. REPAIRED FRAME IAW L-188 SRM 53-2-3, FIG 2. (M)
- [SDR ZIAA04054](https://openairdocs.org/sdr/ZIAA04054), Sep 6, 2001: FRAME. CRACKED. YIP - FOUND FUSELAGE FRAME CRACKED AT FS 401, STRINGER 8. REPAIRED FRAME AT STRINGER 8 PER L-188 SRM 53-2-3 FIG 2. (M)
- [SDR ZIAA04042](https://openairdocs.org/sdr/ZIAA04042), Sep 6, 2001: FRAME. CRACKED. FOUND FUSELAGE FRAME CRACKED AT FS 407 BETWEEN STRINGERS 1-2. REPAIRED FRAME AT STRINGER 1-2 PER L188 SRM 53-2-3, FIG 2. (M)
- [SDR ZIAA04041](https://openairdocs.org/sdr/ZIAA04041), Sep 6, 2001: FRAME. CRACKED. YIP - FOUND FUSELAGE FRAME CRACKED AT FS 388 BETWEEN STRINGERS 72-1. REPAIRED FRAME AT STRINGER 72-1 PER LOCKHEED S/B 706 DWG 842354. (M)
- [SDR ZIAA04053](https://openairdocs.org/sdr/ZIAA04053), Sep 6, 2001: FRAME. CRACKED. YIP - FOUND FUSELAGE FRAME CRACKED AT FS 407, STRINGER 8. REPAIRED FRAME AT STRINGER 8 PER L-188 SRM 53-2-3, FIG 2. (M)
- [SDR ZIAA04048](https://openairdocs.org/sdr/ZIAA04048), Sep 6, 2001: FRAME. CRACKED. YIP - FOUND FUSELAGE FRAME CRACKED AT FS 578 BETWEEN STRINGERS 72-1. REPAIRED FRAME AT STRINGER 72-1 IAW L-188 SRM 53-2-3 FIG 2. (M)
- [SDR ZIAA04047](https://openairdocs.org/sdr/ZIAA04047), Sep 6, 2001: FRAME. CORRODED. FOUND LIGHT CORROSION ON FRAME AT FS 540 STRINGER 69. REMOVED CORROSION AND REPAIRED FRAME PER L-188 SRM 53-2-3, FIG 2. PLUGGED NEGLIBIBLE HOLES PER L-188 SRM 5
- [SDR ZIAA04046](https://openairdocs.org/sdr/ZIAA04046), Sep 6, 2001: FRAME. CRACKED. YIP - FOUND FUSELAGE FRAME CRACKED AT FS 464 AT STRINGER 70-71. REPAIRED FRAME AT STRINGER 70-71 IAW L-188 SRM 53-2-3, FIG 2. (M)
- [SDR ZIAA04045](https://openairdocs.org/sdr/ZIAA04045), Sep 6, 2001: FRAME. CRACKED. YIP - FOUND FUSELAGE FRAME CRACKED AT FS 426 AT STRINGER 71. REPAIRED FRAME AT FS 426 FROM STRINGER 68-4 IAW L-188 SRM 53-2-3. (M)
- [SDR ZIAA04051](https://openairdocs.org/sdr/ZIAA04051), Sep 6, 2001: FRAME. CRACKED. YIP - FOUND FUSELAGE FRAME CRACKED AT FS 730, STRINGER 72. REPAIRED FRAME AT STRINGER 72 PER L-188 S/B 706 DWG 842354. (M)
- [SDR ZIAA04052](https://openairdocs.org/sdr/ZIAA04052), Sep 6, 2001: FRAME. CRACKED. FOUND FUSELAGE FRAME CRACKED AT FS 920 BETWEEN STRINGERS 67-69. REPAIRED FRAME AT STRINGER 66-69 PER L-188 SRM 53-2-3, FIG 2. (M)
- [SDR ZIAA04044](https://openairdocs.org/sdr/ZIAA04044), Sep 6, 2001: FRAME. CRACKED. FOUND FUSELAGE FRAME CRACKED AT FS 426 AT STRINGER 1. REPAIRED FRAME AT FS 426 FROM STRINGER 68-4 IAW L-188 SRM 53-2-3. (M)
- [SDR ZIAA04001](https://openairdocs.org/sdr/ZIAA04001), Jul 30, 2001: DOUBLER. CRACKED. FOUND WS 249 LOWER SURFACE, LEAP DOUBLER AT FORWARD EDGE IS CRACKED AT RIGHT WING. ROUTED OUT DEFECTIVE AREA OF LEAP DOUBLER. DYE PEN OF WING PLANK REVEALED NO 
- [SDR ZIAA04003](https://openairdocs.org/sdr/ZIAA04003), Jul 30, 2001: DOUBLER. CRACKED. FOUND LOWER SURFACE AT WS 265 RIGHT WING LEAP DOUBLER ON PLANK NR 4 IS CRACKED. LEAK CHECK DUE. ROUTED OUT CRACKED LEAP DOUBLER MATERIAL. INSPECTED WING PLANK S
- [SDR ZIAA04002](https://openairdocs.org/sdr/ZIAA04002), Jul 30, 2001: DOUBLER. CRACKED. YIP - FOUND LWER SURFACE AT WS 253, FORWARD EDGE OF LEAP DOUBLER IS CRACKED, RIGHT WING. CRACK STOP DRILLED, ROUTED OUT DEFECTIVE AREA OF LEAP DOUBELR. DYE PEN 
- [SDR ZIAA98011](https://openairdocs.org/sdr/ZIAA98011), Sep 14, 1998: SKIN. CORRODED. YIP - POPPED RIVETS RIGHT SIDE, FORWARD OF BELLY DOOR CUTOUT. REMOVED CORRODED SECTION OF FUSELAGE SKIN AT RFS 200 TO 237.5. REPAIRED SKIN BY REPLACING SKIN FRO
- [SDR ZIAA98002](https://openairdocs.org/sdr/ZIAA98002), Jan 18, 1998: ENGINE. FAILED. CYYT - UPON APPROACH INTO CYYT, NR 1 ENIGNE RPM DECAYED TO ZERO, PULLED SHUTDOWN HANDLE. MAINTENANCE INSPECTION REVEALED NR 1 ENGINE APPEARS TO BE DE-COUPLED. A
- [SDR ZIAA96036](https://openairdocs.org/sdr/ZIAA96036), May 11, 1996: SKIN. CORRODED. YIP - DURING INSPECTION UPPER RIGHT WING, PLANK NR 4 AT 3/4 PLANK SEAM CRACKED BETWEEN STATION 328 AND 330. REPAIRED AS PER L-188 LOCKHEED BS 620 DRAWING NR 841
- [SDR ZIAA96035](https://openairdocs.org/sdr/ZIAA96035), May 11, 1996: SKIN. CORRODED. YIP - DURING INSPECTION, LOWER RIGHT WING, PLANK NR 1 AT 1/2 PLANK SEAM CRACKED BETWEEN STATION 111 AND 112.5. REPAIRED AS PER L-188 SRM 57-2-1 PG 30. (M)
- [SDR ZIAA96034](https://openairdocs.org/sdr/ZIAA96034), May 11, 1996: SKIN. CRACKED. YIP - DURING INSPECTION, UPPER RIGHT WING, PLANK NR 8 AT 7/8 PLANK SEAM CRACKED BETWEEN STATION 69 AND 83. CLEAN UP AREA OUT OF LIMITS. REPAIRED PLANK AS PER DE
- [SDR ZIAA96033](https://openairdocs.org/sdr/ZIAA96033), May 11, 1996: SKIN. CRACKED. YIP - DURING INSPECTION, UPPER RIGHT WING, PLANK NR 7 AT 6/7 PLANK SEAM CRACKED BETWEEN STATION 69 AND 79. REPAIRED AS PER L-188 LOCKHEED SB 678 DRAWING NR 8424
- [SDR ZIAA96032](https://openairdocs.org/sdr/ZIAA96032), May 11, 1996: SKIN. CRACKED. YIP - DURING INSPECTION, UPPER RIGHT WING, PLANK NR 6 AND 5/6 PLANK SEAM CRACKED BETWEEN STATION 74 AND 82. REPAIRED AS PER L-188 LOCKHEED SB 678 DRAWING NR 842
- [SDR ZIAA96031](https://openairdocs.org/sdr/ZIAA96031), May 11, 1996: SKIN. CRACKED. YIP - DURING INSPECTION, UPPER RIGHT WING, PLANK NR 5 AT 4/5 PLANK SEAM CRACKED BETWEEN STATION 90 AND 92. REPAIRED AS PER L-188 SRM 57-2-1 PG 33 AND LOCKHEED S
- [SDR ZIAA96030](https://openairdocs.org/sdr/ZIAA96030), May 11, 1996: SKIN. CRACKED. YIP - DURING INSPECTION, UPPER RIGHT WING, PLANK NR 5 AT 4/5 PLANK SEAM CRACKED BETWEEN STATION 75 AND 78. REPAIRED AS PER L-188 SRM 57-2-1 PG 33 AND LOCKHEED S
- [SDR ZIAA96029](https://openairdocs.org/sdr/ZIAA96029), May 11, 1996: SKIN. CORRODED. YIP - DURING INSPECTION, UPPER RIGHT, PLANK NR 2 AT 2/3 PLANK SEAM CRACKED BETWEEN STATION 86 AND 88. REPAIRED AS PER L-188 SRM 57-2-1 PG 33. (M)
- [SDR ZIAA96028](https://openairdocs.org/sdr/ZIAA96028), May 11, 1996: SKIN. CORRODED. YIP - DURING INSPECTION, UPPER RIGHT WING, PLANK NR 2 AT 2/3 PLANK SEAM CRACKED BETWEEN STATION 76.5 AND 79. REPAIRED AS PER L-188 SRM 57-2-1 PG 33. (M)
- [SDR ZIAA96027](https://openairdocs.org/sdr/ZIAA96027), May 11, 1996: SKIN. CORRODED. YIP - DURING INSPECTION UPPER RIGHT WING, PLANK NR 1 AT 1/2 PLANK SEAM CRACKED BETWEEN STATION 71.5 AND 73. REPAIRED AS PER L-188 LOCKHEED SB 678 DRAWING NR 842
- [SDR ZIAA96026](https://openairdocs.org/sdr/ZIAA96026), May 11, 1996: SKIN. CORRODED. YIP - DURING INSPECTION UPPER LEFT WING, PLANK NR 6 AT 5/6 PLANK SEAM CRACKED BETWEEN STATION 77 AND 80. CLEAN UP AREA OUT OF LIMITS. REPAIRED PLANK AS PER ZIAA
- [SDR ZIAA96025](https://openairdocs.org/sdr/ZIAA96025), May 11, 1996: SKIN. CRACKED. YIP - DURING INSPECTION UPPER RT WING, PLANK NR 4 AT 4/5 PLANK SEAM CRACKED AT STATION 80 3.5 INCH FORWARD OF PLANK SEAM. REPAIRED PLANK AS PER L-188 SRM 57-2-1
- [SDR ZIAA96024](https://openairdocs.org/sdr/ZIAA96024), May 11, 1996: SKIN. CORRODED. YIP - DURING INSPECTION UPPER RT WING, PLANK NR 7 AT 6/7 PLANK SEAM CRACKED BETWEEN STATION 249 AND 252. CLEAN UP AREA OUT OF LIMITS. REPAIRED PLANK AS PER ZIAA
- [SDR ZIAA96023](https://openairdocs.org/sdr/ZIAA96023), May 10, 1996: SKIN. CRACKED. YIP - DURING INSPECTION UPPER LEFT WING, PLANK NR 7 AT 6/7 PLANK SEAM CRACKED BETWEEN STATION 121.5 AND 124.5. REPAIRED AS PER L-188 SRM 57-2-1 PG 33. (M)
- [SDR ZIAA96022](https://openairdocs.org/sdr/ZIAA96022), May 10, 1996: SKIN. CORRODED. YIP - DURING INSPECTION LOWER LEFT WING, PLANK NR 3 AT 2/3 PLANK SEAM CRACKED BETWEEN STATION 244 AND 246. CLEAN UP AREA OUT OF LIMITS. REPAIRED PLANK AS PER L-
- [SDR ZIAA96021](https://openairdocs.org/sdr/ZIAA96021), May 10, 1996: SKIN. CORRODED. YIP - DURING INSPECTION UPPER LEFT WING, PLANK NR 4 AT 3/4 PLANK SEAM CRACKED BETWEEN STATION 190 AND 193. CLEAN UP AREA OUT OF LIMITS. REPAIRED PLANK AS PER 18
- [SDR ZIAA96020](https://openairdocs.org/sdr/ZIAA96020), May 10, 1996: SKIN. CORRODED. YIP - DURING INSPECTION UPPER LEFT WING, PLANK NR 4 AT 3/4 PLANK SEAM CRACKED BETWEEN STATION 73.5 AND 79.5. CLEAN UP AREA OUT OF LIMITS. REPAIRED PLANK AS PER 

## STCs that may be installed (OpenAirDocs) (89, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Lockheed 188C)

- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST00353LA](https://openairdocs.org/stc/ST00353LA): Installation of a 3000 gallon retardant tank system. Air Spray USA Inc
- [STC ST02636LA](https://openairdocs.org/stc/ST02636LA): Modification to upgrade the existing XS-950 Mode S Transponder system to add ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA2197WE](https://openairdocs.org/stc/SA2197WE): Installation of Brownline modified cargo restraint system. Telair US LLC
- [STC SA3675WE](https://openairdocs.org/stc/SA3675WE): Installation of Brownline cargo system P/N 46234-101. Telair US LLC
- [STC ST02524LA](https://openairdocs.org/stc/ST02524LA): Installation of TCAS version 7.0. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA2324WE](https://openairdocs.org/stc/SA2324WE): Installation of spraymat ice protection system on L-188 propeller spinner, Hamilton Standard P/N 553546, replacing Hamilton Standard heater blanket. ROBERT W. MURRAY
- [STC ST00986LA-D](https://openairdocs.org/stc/ST00986LA-D): Installation of lower cargo compartment smoke detection system provisions. Ontic Engineering and Manufacturing Inc
- [STC SA1081SO](https://openairdocs.org/stc/SA1081SO): Increase in fuel weight from86,000 pounds to 92,340 pounds. Aeronautical Engineers Inc
- [STC ST508SO](https://openairdocs.org/stc/ST508SO): Installation of lap/shoulder belts. Aeronautical Engineers Inc
- [STC ST885SO](https://openairdocs.org/stc/ST885SO): Modification to a cargo configuration. Aeronautical Engineers Inc
- [STC SA7772SW](https://openairdocs.org/stc/SA7772SW): Replacement of existing torquemeters. AVMAR a Michigan Corporation
- [STC SA1637WE](https://openairdocs.org/stc/SA1637WE): Installation of cargo door approximately 80 inches high by 144 inches long in left side of fuselage forebody. Lockheed Martin Aeronautics Company
- [STC SA1754WE](https://openairdocs.org/stc/SA1754WE): Installation of cargo doors, cargo floor and other changes. (188A, 188C Aircraft SN 1070 and higher are eligible.). Lockheed Martin Aeronautics Company
- [STC SA4-1403](https://openairdocs.org/stc/SA4-1403): Installation of a Lockheed Aircraft Service model 109C flight data recorder. Lockheed Martin Aeronautics Company
- [STC SA707EA](https://openairdocs.org/stc/SA707EA): Relocation of cabin window right-side from fuselage station 217-236 to fuselage station 333-352. Lockheed Martin Aeronautics Company
- [STC SA708EA](https://openairdocs.org/stc/SA708EA): Installation of opening in fuselage right hand for emergency exit between fuselage station 226 and fuselage station 253.4. Is approved only for its structural, electrical and mechanical provisions and can be incorporated with STC SA707EA and STC SA709EA. Lockheed Martin Aeronautics Company
- [STC SA709EA](https://openairdocs.org/stc/SA709EA): Installation of floor structure and miscellaneous modifications. Is approved only for its structural and electrical provisions and can be incorporated with STC SA707EA and SA708EA. Lockheed Martin Aeronautics Company
- [STC ST01836NY](https://openairdocs.org/stc/ST01836NY): Three Man to Two Man Crew Conversion. Cascade Aerospace Inc
- [STC ST01004NY](https://openairdocs.org/stc/ST01004NY): Installation of cargo restraint straps. Airline Container Manufacturing Co Inc
- [STC ST02035AK](https://openairdocs.org/stc/ST02035AK): Installation of Honeywell TCAS II. ACSS (Aviation Communication and Surveillance Syst
- [STC SA2405WE](https://openairdocs.org/stc/SA2405WE): Installation of PICO Division pressure regulator P/N 3001 on automatically inflatable emergency evacuation slides in lieu of International Inflatables pressure regulator P/N 68240 and 70003. Goodrich Corporation
- [STC SA1060GL](https://openairdocs.org/stc/SA1060GL): Installation of Norton Radome Kit4306CX. Saint-Gobain Performance Plastics Corp
- [STC SA1149SW](https://openairdocs.org/stc/SA1149SW): Installation of a hot water heater. Signature Flight Support Corporation
- [STC SA1150SW](https://openairdocs.org/stc/SA1150SW): Installation of Litton LTN 51 inertial navigation system. Signature Flight Support Corporation
- [STC SA2301WE](https://openairdocs.org/stc/SA2301WE): Installation of emblem light. DeVore Aviation Corporation of America, a New Mexico Corporation
- [STC SA2974WE](https://openairdocs.org/stc/SA2974WE): Modification for installation of aft galley and forward galley rework. DeVore Aviation Corporation of America, a New Mexico Corporation
- [STC ST01136AT](https://openairdocs.org/stc/ST01136AT): Modification of Lockheed Electra, Foote-Brothers Mfg. two-speed gear box P/N 50701-1, -2, -3, or -4. Zantop Intl Airlines Inc
- [STC ST02004AK](https://openairdocs.org/stc/ST02004AK): Installation of a Dual Bendix/King MLS-21 microwave landing system. Reeve Aleutian Airways, Inc
- [STC SA218WE](https://openairdocs.org/stc/SA218WE): Turbine installation GTC 85-90E or GTCP 85-291E. AlliedSignal Aviation Services
- [STC SA3120WE](https://openairdocs.org/stc/SA3120WE): Modification consisting of installation of cargo pallet restraint system. (188A s/n 1035 and up). Pemco Engineers Inc
- [STC SA5502NM](https://openairdocs.org/stc/SA5502NM): Modification of Lockheed model L-188A/L-188C airplanes. Channel Express(Air Serviced) Ltd
- [STC SA3117SO](https://openairdocs.org/stc/SA3117SO): Installation of an engine reduction gearbox electrical/magnetic chip detector system. Zantop Intl Airlines Inc
- [STC SA3118SO](https://openairdocs.org/stc/SA3118SO): Installation of fuel flowmeters and a fuel management system. Zantop Intl Airlines Inc
- [STC SA1833SO](https://openairdocs.org/stc/SA1833SO): Installation of an aft cargo door and cargo compartment interior. Universal Cargo Doors & Serv, Inc
- [STC SA1834SO](https://openairdocs.org/stc/SA1834SO): Installation of a forward cargo door and cargo compartment interior. Universal Cargo Doors & Serv, Inc
- [STC SA1506GL](https://openairdocs.org/stc/SA1506GL): Rebuilt alternate flap drive torque tube assembly P/N 807723-R, rebuilt Lockheed P/N 807723 with 4130 tubing and type design end fittings. Zantop Intn'l Airlines Inc
- [STC SA1506GL;](https://openairdocs.org/stc/SA1506GL%3B): Rebuilt alternate flap drive torque tube assembly P/N 807723-R, rebuilt Lockheed P/N 807723 with 4130 tubing and type design end fittings. Zantop Intn'l Airlines, Inc
- [STC SA4925NM](https://openairdocs.org/stc/SA4925NM): Installation of horse containers. Instone Airline Ltd
- [STC SA3148WE](https://openairdocs.org/stc/SA3148WE): Installation of Collins FPC-75 ground proximity warning system. US Airways, Inc
- [STC SA2043SO](https://openairdocs.org/stc/SA2043SO): Installation of dual Sperry SPI-402, flight director system. Zantop Intl Airlines Inc
- [STC SA2012SO](https://openairdocs.org/stc/SA2012SO): Installation of a divider and a courier seat. Spirit America Airlines
- [STC SA835GL](https://openairdocs.org/stc/SA835GL): Modification of underwing fuel quantity gages, Accessory Prod. Co. P/N 727100 (Lockheed P/N LAC 634063) by removing spring and poppet valve and installing a petcock P/N CCA-1550 (TSO-C76). Zantop Intn'l Airlines, Inc
- [STC SA1495SO](https://openairdocs.org/stc/SA1495SO): Modification of Flight Equip. and Engrg. double passenger seat model650L to attach a double shoulder harness/lap belt assembly. Survival Products Inc
- [STC SA533GL](https://openairdocs.org/stc/SA533GL): Install a smoke elimination door. Zantop Intn'l Airlines, Inc
- [STC SA796EA](https://openairdocs.org/stc/SA796EA): Installation of six-seat pallet. Evergreen Air Center Inc
- [STC SA3618WE](https://openairdocs.org/stc/SA3618WE): Relocation of forward airstair to rear left hand type 1 exit. American Jet Industries
- [STC ST754SO](https://openairdocs.org/stc/ST754SO): Installation of remote control essential A-C bus normal and alternate electrical circuit breaker system. MCA Leasing Corp
- [STC SA399NW](https://openairdocs.org/stc/SA399NW): Modify type design by installation of Sorm Bulk Liquid Cargo Tank Assembly SI-9101. Sorm Inc

All 89: https://openairdocs.org/aircraft/N286F/stcs.md

## Related

- Other Lockheed 188C aircraft: https://openairdocs.org/model/lockheed-188c/aircraft.md
- The Allison 501-D13 series engine: https://openairdocs.org/engine/allison-501-d13-series.md

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