# Service difficulty reports: N286F A list on [N286F](https://openairdocs.org/aircraft/N286F.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR ZIAA04059](https://openairdocs.org/sdr/ZIAA04059.md): Floor Support · corroded · Dec 8, 2003 · N286F · Lkheed 188C · Fuselage Miscellaneous Structure > 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 51-2-14. MATERIAL REMOVED IS PAST NEGLIGIBLE LIMITS. REPAIRED AREA PER L-188 SRM 57-2-1, PAGE 19. R - [SDR ZIAA04058](https://openairdocs.org/sdr/ZIAA04058.md): Door Frame · cracked · Sep 20, 2002 · N286F · Lkheed 188C · Fuselage Main, Structure > 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 INVESTIGATE FUSELAGE SKIN. FOUND EXISTING CRACK WAS STOP DRILLED PER L-188 SRM 53-2-1, FIG 2, SHEET 6. R - [SDR ZIAA04057](https://openairdocs.org/sdr/ZIAA04057.md): Skin · corroded · Nov 27, 2001 · N286F · Lkheed 188C · Wing, Plate/Skin > 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 REPAIR PER ZANTOP DWG A72-R03. REMOVED EXTERNAL DOUBLERS ON PLANK 7/8 SEAM AT WS 65-83. CONFIRM CORR - [SDR ZIAA04050](https://openairdocs.org/sdr/ZIAA04050.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame > 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.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame > 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.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame > 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.md): Floorbeam · corroded · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Floor Beam > 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 53-2-4, FIG 2 SHEET 1. (M) - [SDR ZIAA04055](https://openairdocs.org/sdr/ZIAA04055.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame > 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.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame > 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.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame > 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.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame > 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.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame > 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.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame > 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.md): Frame · corroded · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame > 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 51-3-6, FIG 1. (M) - [SDR ZIAA04046](https://openairdocs.org/sdr/ZIAA04046.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame > 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.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame > 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.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame > 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.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame > 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.md): Frame · cracked · Sep 6, 2001 · N286F · Lkheed 188C · Fuselage Main, Frame > 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.md): Doubler · cracked · Jul 30, 2001 · N286F · Lkheed 188C · Wing, Plate/Skin > 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 DISCREPANCIES. REPAIRED IAW L188 SRM 57-2-1 AND SEALED INTERNALLY. (M) - [SDR ZIAA04003](https://openairdocs.org/sdr/ZIAA04003.md): Doubler · cracked · Jul 30, 2001 · N286F · Lkheed 188C · Wing, Plate/Skin > 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 SURFACE WITH DYE PEN. NO DEFECTS FOUND. REPAIRED PER L-188 SRM 57-2-1, FIG 3, SHEET 30, TYPE 2. - [SDR ZIAA04002](https://openairdocs.org/sdr/ZIAA04002.md): Doubler · cracked · Jul 30, 2001 · N286F · Lkheed 188C · Wing, Plate/Skin > 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 OF WING PLANK REVEALED NO DISCREPANCIES. REPAIRED IAW L-188 SRM 57-2-1 AND SEALED INTERNALLY. (M - [SDR ZIAA98011](https://openairdocs.org/sdr/ZIAA98011.md): Skin · corroded · Sep 14, 1998 · N286F · Lkheed 188C · Fuselage Main, Plate/Skin > 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 FROM STATION 200 TO 237.5 AS PER L-188 SRM 53-2-1 PAGE 9 FIG 2 SHEET 2. (M) - [SDR ZIAA98002](https://openairdocs.org/sdr/ZIAA98002.md): Engine · failed · Jan 18, 1998 · N286F · Lkheed 188C · Engine (Turbine/Turboprop) > 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. AIRCRAFT THREE ENGINED FERRIED TO YIP, FOR NR 1 ENGINE REPLACEMENT. ENGINE WAS REPLACED ON 1-28-98 - [SDR ZIAA96036](https://openairdocs.org/sdr/ZIAA96036.md): Skin · corroded · May 11, 1996 · N286F · Lkheed 188C · Wing, Plate/Skin > 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 841403. (M) - [SDR ZIAA96035](https://openairdocs.org/sdr/ZIAA96035.md): Skin · corroded · May 11, 1996 · N286F · Lkheed 188C · Wing, Plate/Skin > 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.md): Skin · cracked · May 11, 1996 · N286F · Lkheed 188C · Wing, Plate/Skin > 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 DER APPROVED ZIAA DRAWING NR A72-R03. (M) - [SDR ZIAA96033](https://openairdocs.org/sdr/ZIAA96033.md): Skin · cracked · May 11, 1996 · N286F · Lkheed 188C · Wing, Plate/Skin > 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 842451. (M) - [SDR ZIAA96032](https://openairdocs.org/sdr/ZIAA96032.md): Skin · cracked · May 11, 1996 · N286F · Lkheed 188C · Wing, Plate/Skin > 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 842451. (M) - [SDR ZIAA96031](https://openairdocs.org/sdr/ZIAA96031.md): Skin · cracked · May 11, 1996 · N286F · Lkheed 188C · Wing, Plate/Skin > 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 SB 678 DRAWING NR 842451. (M) - [SDR ZIAA96030](https://openairdocs.org/sdr/ZIAA96030.md): Skin · cracked · May 11, 1996 · N286F · Lkheed 188C · Wing, Plate/Skin > 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 SB 678 DRAWING NR 842451. (M) - [SDR ZIAA96029](https://openairdocs.org/sdr/ZIAA96029.md): Skin · corroded · May 11, 1996 · N286F · Lkheed 188C · Wing, Plate/Skin > 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.md): Skin · corroded · May 11, 1996 · N286F · Lkheed 188C · Wing, Plate/Skin > 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.md): Skin · corroded · May 11, 1996 · N286F · Lkheed 188C · Wing, Plate/Skin > 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 842451. (M) - [SDR ZIAA96026](https://openairdocs.org/sdr/ZIAA96026.md): Skin · corroded · May 11, 1996 · N286F · Lkheed 188C · Wing, Plate/Skin > 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 DER APPROVED DRAWING NR A72-R05. (M) - [SDR ZIAA96025](https://openairdocs.org/sdr/ZIAA96025.md): Skin · cracked · May 11, 1996 · N286F · Lkheed 188C · Wing, Plate/Skin > 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 PG 17. (M) - [SDR ZIAA96024](https://openairdocs.org/sdr/ZIAA96024.md): Skin · corroded · May 11, 1996 · N286F · Lkheed 188C · Wing, Plate/Skin > 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 DER APPROVED DRAWING NR A72-R02. (M) - [SDR ZIAA96023](https://openairdocs.org/sdr/ZIAA96023.md): Skin · cracked · May 10, 1996 · N286F · Lkheed 188C · Wing, Plate/Skin > 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.md): Skin · corroded · May 10, 1996 · N286F · Lkheed 188C · Wing, Plate/Skin > 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-188 SRM 57-2-1 PG 33 AND 37. (M) - [SDR ZIAA96021](https://openairdocs.org/sdr/ZIAA96021.md): Skin · corroded · May 10, 1996 · N286F · Lkheed 188C · Wing, Plate/Skin > 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 188 SRM AND DER APPROVED ZIAA DRAWING NR A72-R01. (M) - [SDR ZIAA96020](https://openairdocs.org/sdr/ZIAA96020.md): Skin · corroded · May 10, 1996 · N286F · Lkheed 188C · Wing, Plate/Skin > 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 DER APPROVED ZIAA DRAWING NR A72-R04. (M) ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N286F' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N286F/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.