# Service difficulty reports: N35888, cancelled May 12, 2003 A list on [N35888, cancelled May 12, 2003](https://openairdocs.org/deregistered/N35888-2003-05-12.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 3 · 119 reports - [SDR CALA0001634](https://openairdocs.org/sdr/CALA0001634.md): Cargo Track · corroded · Oct 23, 2000 · N35888 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND AFT CARGO LT TIE DOWN TRACK CORRODED UNDER CLIP NUTS AT FS 1230 - 1322. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-10-4, 51-10-3, AND 53-05, FIGURE 3. - [SDR CALA0001633](https://openairdocs.org/sdr/CALA0001633.md): Doubler · cracked · Oct 23, 2000 · N35888 · Doug DC982 · Fuselage Main, Bulkhead > INSPECTION FOUND A 2 INCH CRACK IN DOUBLER AT RT WHEEL WELL FORWARD LOWER CORNER. REMOVED INTERCOSTAL AND DOUBLER AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-04 AND 53-30-5. - [SDR CALA0001632](https://openairdocs.org/sdr/CALA0001632.md): Cargo Track · corroded · Oct 23, 2000 · N35888 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND FORWARD CARGO AFT RT TIE DOWN TRACK HAD CORRODED SCREW HOLES ON TOP AND BOTTOM. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 51-30-1, 51-30-3, AND 51-30-4. - [SDR CALA0001631](https://openairdocs.org/sdr/CALA0001631.md): Cargo Track · corroded · Oct 23, 2000 · N35888 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND AFT CARGO RT SIDE TIE DOWN TRACK CORRODED BETWEEN FS 1212 - 1322. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-05, FIGURE 4 AND 51-10-3. - [SDR CALA0001619](https://openairdocs.org/sdr/CALA0001619.md): Skin · gouged · Oct 21, 2000 · N35888 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND RT AFT EMERGENCY EXIT DOOR CUTOUT SKIN GOUGED AT UPPER DOOR LATCH. THE RIVETS WERE REMOVED IAW SRM 51-30-2. THE SEAL DEPRESSOR WAS CUT IAW SRM 53-05, FIGURE 32. A REPAIR ANGLE WAS INSTALLED IAW SRM 51-10-4 AND 53-05, FIGURE 32. - [SDR CALA0001618](https://openairdocs.org/sdr/CALA0001618.md): Cargo Track · corroded · Oct 21, 2000 · N35888 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LT TIE DOWN TRACK IN AFT CARGO AREA CORRODED BETWEEN FS 1007 AND 1320. THE TIE DOWN TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 4G. - [SDR CALA0001617](https://openairdocs.org/sdr/CALA0001617.md): Cargo Track · corroded · Oct 21, 2000 · N35888 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND AFT RT END OF TRACK TO AFT BULKHEAD FRAME IN FWD CARGO PIT CORRODED AT STA 522. THE TRACK WAS REMOVED AND A NEW SECTION OF TRACK WAS INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-5. - [SDR CALA0001600](https://openairdocs.org/sdr/CALA0001600.md): Floor Support · corroded · Oct 18, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CABIN FLOOR SUPPORT CORRODED BETWEEN FS 160 AND 200, RBL 39. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-03, 51-30-2, AND 51-10-04. - [SDR CALA0001599](https://openairdocs.org/sdr/CALA0001599.md): Support Bracket · cracked · Oct 18, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 6 INCH CRACK IN CENTER KEEL SUPPORT AT STA 948. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-01 AND 53-01. - [SDR CALA0001598](https://openairdocs.org/sdr/CALA0001598.md): Angle · cracked · Oct 18, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 6 INCH CRACK IN ANGLE JUST FORWARD OF RUDDER TRIM ACTUATOR IN TAIL COMPARTMENT AREA AT STA 1485, RT SIDE. THE VENT BOX WAS REMOVED IAW SRM 51-30-1. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS INSTALLED IAW SRM 51-30-5. THE VENT BOX WAS REIN - [SDR CALA0001595](https://openairdocs.org/sdr/CALA0001595.md): Intercostal · corroded · Oct 17, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND INTERCOSTAL AND ATTACHING BRACKETS CORRODED IN AFT CARGO AREA BETWEEN FS 1148 - 1155, LONGERONS 29R AND 30. THE INTERCOSTAL AND BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-2. - [SDR CALA0001594](https://openairdocs.org/sdr/CALA0001594.md): Floor Support · corroded · Oct 17, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT FS 180, LBL 12 - 37. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA0001593](https://openairdocs.org/sdr/CALA0001593.md): Intercostal · cracked · Oct 17, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 1 INCH CRACK AT AFT END LOWER SIDE OF AFT ACCESSORY COMPARTMENT INTERCOSTAL BETWEEN FS 1497 AND 1510. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-2. - [SDR CALA0001592](https://openairdocs.org/sdr/CALA0001592.md): Floor Support · corroded · Oct 17, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CABIN FORWARD ENTRY FLOOR SUPPORT CORRODED BETWEEN FS 160 AND 190, LBL 40. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-10-4, 51-30-2, AND 51-30-5, PAGE 1. - [SDR CALA0001589](https://openairdocs.org/sdr/CALA0001589.md): Floorbeam · cracked · Oct 16, 2000 · N35888 · Doug DC982 · Fuselage Main, Floor Beam > INSPECTION FOUND A 2 INCH CRACK IN FLOORBEAM AT FS 218, LBL 44. THE FLOORBEAM WAS REMOVED AND A NEW FLOORBEAM WAS INSTALLED IAW 53-05, FIGURE A AND 51-30-2. - [SDR CALA0001585](https://openairdocs.org/sdr/CALA0001585.md): Pan · corroded · Oct 15, 2000 · N35888 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND FORWARD CARGO DOOR JAMB PAN CORRODED BETWEEN FS 370 AND 427. THE DOOR PAN WAS REPLACED IAW SRM 51-30-2. THE OUTSIDE LOWER SCUFF PLATE WAS REPLACED IAW SRM 51-30-3. - [SDR CALA0001584](https://openairdocs.org/sdr/CALA0001584.md): Cargo Track · corroded · Oct 15, 2000 · N35888 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND RT CARGO TIEDOWN TRACK CORRODED IN AFT CARGO AREA AT FS 1007 - 1155. THE TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW SRM 53-04, FIGURE 4. - [SDR CALA0001583](https://openairdocs.org/sdr/CALA0001583.md): Intercostal · corroded · Oct 15, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT CARGO CHANNEL INTERCOSTAL CORRODED ON DOOR JAMB. THE INTERCOSTAL WAS REMOVED AND A NEW INTERCOSTAL WAS INSTALLED IAW SRM 51-10-2 AND 51-30-05. - [SDR CALA0001582](https://openairdocs.org/sdr/CALA0001582.md): Support Bracket · corroded · Oct 15, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND LOWER BULKHEAD SUPPORT CORRODED IN AFT CARGO AREA AT FS 1322. THE SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-10-4 AND 51-30-2. - [SDR CALA0001581](https://openairdocs.org/sdr/CALA0001581.md): Intercostal · gouged · Oct 15, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A GOUGE IN RADIUS OF INTERCOSTAL AND CORROSION WAS NOTED BETWEEN FASTENERS ON LOWER ANGLE MATING SKIN AT FS 430 - 446, L28R. THE INTERCOSTAL WAS REMOVED AND A NEW ONE WAS INSTALLED IAW SRM 51-30-5. - [SDR CALA0001577](https://openairdocs.org/sdr/CALA0001577.md): Floor Support · corroded · Oct 14, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT CARGO FLOOR SUPPORT CORRODED AT FS 1117 - 1155 BETWEEN L28L AND L28R. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW 51-30-2 AND 51-30-5. - [SDR CALA0001576](https://openairdocs.org/sdr/CALA0001576.md): Floor Support · corroded · Oct 14, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORT CORRODED AT FS 180, RBL 9 TO RBL 38. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-2 AND 51-10-4. - [SDR CALA0001568](https://openairdocs.org/sdr/CALA0001568.md): Finger Doubler · corroded · Oct 13, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND SKIN FINGER DOUBLER CORRODED AT FS 256, LONGERON 26L. THE FINGER DOUBLER WAS REMOVED AND A NEW FINGER DOUBLER WAS INSTALLED IAW SRM 51-10-3 AND EA 9-5332-2-A0790. - [SDR CALA0001567](https://openairdocs.org/sdr/CALA0001567.md): Angle · corroded · Oct 13, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND MID CARGO RT TRACK FLOOR SUPPORT Z-ANGLE CORRODED AT FS 586 - 636. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 53-01, FIGURE 1. - [SDR CALA0001566](https://openairdocs.org/sdr/CALA0001566.md): Plate · corroded · Oct 13, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT CARGO CENTER THRESHOLD PLATE CORRODED AT STA 1231. THE THRESHOLD PLATE REMOVED AND REPLACED IAW SRM 51-10-3. - [SDR CALA0001565](https://openairdocs.org/sdr/CALA0001565.md): Floor Support · corroded · Oct 13, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND R-1 DOOR ENTRY FLOOR SUPPORT CORRODED AT FS 155 - 200. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 51-30-1. - [SDR CALA0001564](https://openairdocs.org/sdr/CALA0001564.md): Intercostal · cracked · Oct 13, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AN 8 INCH CRACK IN INTERCOSTAL AT SUB FLOOR INSIDE L-1 DOOR, FS 190, LBL 56. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-10-3 AND 51-30-2. - [SDR CALA0001563](https://openairdocs.org/sdr/CALA0001563.md): Web · cracked · Oct 13, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND A 19 INCH CRACK IN CABIN RT CUSP WEB AT FS 218 - 237, RBL 44 - 54. THE CUSP WEB WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. - [SDR CALA0001562](https://openairdocs.org/sdr/CALA0001562.md): Cargo Track · corroded · Oct 13, 2000 · N35888 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND MID PIT LT TIE DOWN TRACK CORRODED AT FASTENER HOLES FROM FS 541 - 790. THE TIE DOWN TRACK WAS REMOVED AND A NEW TRACK WAS INSTALLED IAW 51-30-2, 51-10-3, AND 51-30-5. - [SDR CALA0001561](https://openairdocs.org/sdr/CALA0001561.md): Floor Support · corroded · Oct 13, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FLOOR SUPPORTS CORRODED AT FS 200, RBL 4 TO LBL 4, LBL 8, AND RBL 10 TO 40. THE FLOOR SUPPORTS WERE REMOVED AND NEW FLOOR SUPPORTS WERE INSTALLED IAW SRM 51-30-2, 51-10-3, AND 51-30-5. - [SDR CALA0001560](https://openairdocs.org/sdr/CALA0001560.md): Seat Track · corroded · Oct 13, 2000 · N35888 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND RIGHT I/B CABIN SEAT TRACK CORRODED AT FS 200 - 265. THE SEAT TRACK WAS REMOVED AND A NEW SEAT TRACK WAS INSTALLED IAW SRM 51-30-1. - [SDR CALA0001558](https://openairdocs.org/sdr/CALA0001558.md): Support Fitting · corroded · Oct 12, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT CARGO BULKHEAD CENTER VERTICAL SUPPORT CORRODED AT FS 1322. THE VERTICAL SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-30-5. - [SDR CALA0001557](https://openairdocs.org/sdr/CALA0001557.md): Hinge · corroded · Oct 12, 2000 · N35888 · Doug DC982 · Fluid Service Doors > INSPECTION FOUND AFT LAV SERVICE PANEL ACCESS DOOR HINGE AND BRACKET CORRODED. THE DOOR HINGE AND BRACKET WERE REMOVED AND REPLACED IAW SRM 51-30-5, 51-30-1, AND 51-10-4. - [SDR CALA0001556](https://openairdocs.org/sdr/CALA0001556.md): Fitting · corroded · Oct 12, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT CARGO SUPPORT FITTING CORRODED AT FS 1007, LONGERON 28R. THE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-5. - [SDR CALA0001555](https://openairdocs.org/sdr/CALA0001555.md): Floor Panel · cracked · Oct 12, 2000 · N35888 · Doug DC982 · Fuselage Floor Panel > INSPECTION FOUND A 2 INCH CRACK IN FIRST OFFICER''S SEAT LOWER FLOOR PANEL. THE FLOOR PANEL WAS REMOVED AND A NEW PANEL WAS INSTALLED IAW SRM 51-30-4. - [SDR CALA0001554](https://openairdocs.org/sdr/CALA0001554.md): Galley Track · corroded · Oct 12, 2000 · N35888 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND G-2 GALLEY SUPPORT CORRODED AT FS 218, RBL 11. THE GALLEY SUPPORT WAS REMOVED AND A NEW SUPPORT WAS INSTALLED IAW SRM 51-30-5. - [SDR CALA0001553](https://openairdocs.org/sdr/CALA0001553.md): Rib · corroded · Oct 12, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FUSELAGE FAIRING MOUNTING RIB 5L CORRODED AT BOTTOM LOCATION FS 826, LONGERON 29L. DOUBLERS AND SHIM WERE INSTALLED IAW SRM 53-01, FIGURE 2. - [SDR CALA0001549](https://openairdocs.org/sdr/CALA0001549.md): Skin · cracked · Oct 12, 2000 · N35888 · Doug DC982 · Cargo/Baggage Doors > INSPECTION FOUND TWO CRACKS IN DOUBLER AROUND DOOR HANDLE OF FWD CARGO DOOR OUTER SKIN. THE DOUBLER WAS REMOVED AND A NEW DOUBLER WAS INSTALLED IAW SRM 51-10-3 AND 51-30-2. - [SDR CALA0001548](https://openairdocs.org/sdr/CALA0001548.md): Skin · dented · Oct 12, 2000 · N35888 · Doug DC982 · Fuselage Main, Plate/Skin > INSPECTION FOUND FUSELAGE SKIN DENTED BETWEEN FS 1271 AND 1289 AT LONGERON 27L. THE DENT WAS REFORMED AND A DOUBLER WAS INSTALLED IAW SRM 53-04, FIGURE 38 AND 51-30-2. - [SDR CALA0001537](https://openairdocs.org/sdr/CALA0001537.md): Web · corroded · Oct 10, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND CORROSION UNDER AND ON FORWARD TORQUE BOX STRAP AND WEB AT FS 1155 - 1212. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-3. CORROSION REMOVAL FROM THE STRAP WAS WITHIN LIMITS IAW SRM 53-01, FIGU - [SDR CALA0001536](https://openairdocs.org/sdr/CALA0001536.md): Beam · corroded · Oct 10, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND LOWER HALF OF AFT CARGO DOOR JAMB BEAM CORRODED ON BOTH SIDES AT FS 1155 - 1212. THE BEAM WAS REMOVED AND REPLACED IAW SRM 51-30-2, 51-30-5, 51-10-4, AND 51-10-3. - [SDR CALA0001535](https://openairdocs.org/sdr/CALA0001535.md): Web · corroded · Oct 10, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND WEB CORRODED AT FS 200, RBL 13, AFT OF FLOORBEAM. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED USING A SPLICE IAW SRM 51-10-2 AND 51-30-2. - [SDR CALA0001534](https://openairdocs.org/sdr/CALA0001534.md): Seat Track · corroded · Oct 10, 2000 · N35888 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND LEFT I/B SEAT TRACK CORRODED AT STA 1030 - 1309. FLOOR PANELS WERE REMOVED TO GAIN ACCESS. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 53-05, FIGURE 47. THE FLOOR PANELS WERE REINSTALLED AND SEALED IAW ECRA 5100-01844. - [SDR CALA0001533](https://openairdocs.org/sdr/CALA0001533.md): Channel · corroded · Oct 10, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND ON O/B END OF INSIDE CHANNEL OF THE L-1 DOOR JAMB STRIP. THE CHANNEL WAS REPLACED IAW SRM 51-30-2 AND 51-10-3. - [SDR CALA0001532](https://openairdocs.org/sdr/CALA0001532.md): Floor Support · corroded · Oct 10, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND FORWARD ENTRY FLOOR SUPPORT CORRODED AT FS 160, RBL 7 TO LBL 7. THE FLOOR SUPPORT WAS REMOVED AND A NEW FLOOR SUPPORT WAS INSTALLED IAW SRM 53-14-1. - [SDR CALA0001531](https://openairdocs.org/sdr/CALA0001531.md): Strap · corroded · Oct 10, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND STRAP CORRODED IN AFT PIT AT STA 1184 BETWEEN LONGERONS 29R AND 30. THE STRAP WAS REMOVED AND A NEW STRAP WAS INSTALLED IAW SRM 53-34-0, 51-10-4, 51-10-3, 51-30-2, 51-30-5. - [SDR CALA0001528](https://openairdocs.org/sdr/CALA0001528.md): Web · corroded · Oct 10, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND G-2 GALLEY SUPPORT CUSP WEB CORRODED AT FS 218, RBL 11. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-30-2. - [SDR CALA0001527](https://openairdocs.org/sdr/CALA0001527.md): Seat Track · corroded · Oct 10, 2000 · N35888 · Doug DC982 · Fuselage, Seat/Cargo Attach Fittings > INSPECTION FOUND RIGHT O/B SEAT TRACK CORRODED AT FS 200 - 237. THE SEAT TRACK WAS REMOVED AND REPLACED IAW 53-05, FIGURE 4A. - [SDR CALA0001520](https://openairdocs.org/sdr/CALA0001520.md): Bracket · corroded · Oct 8, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT CARGO TORQUE BOX CHANNEL BRACKET CORRODED IN DOOR JAMB AREA. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-30-5, 51-10-4, AND 51-10-3. - [SDR CALA0001519](https://openairdocs.org/sdr/CALA0001519.md): Intercostal · corroded · Oct 8, 2000 · N35888 · Doug DC982 · Fuselage Miscellaneous Structure > INSPECTION FOUND AFT CARGO T-INTERCOSTAL CORRODED AROUND CLIPNUT HOLES IN DOOR JAMB AREA. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-30-5, 51-10-4, AND 51-10-3. Next page: https://openairdocs.org/deregistered/N35888-2003-05-12/reports.md?page=2 ## 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 = 'N35888' AND deregistration_id = 'N35888-2003-05-12' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N35888-2003-05-12/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.