N8517F
Service difficulty reports · 73
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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 = 'N8517F' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 = 'N8517F' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SWAA2026101985298Oil System · low pressureOIL QUANTITY ZERO. OIL PRESSURE DROP TO RED BOX SHUT DOWN ENG 2. EMER DECLARED, TRUCKS ROLLED. PASSENGERS WERE FINE. R & R #2 ENGINE REF. MT 771-00-01.SDR SWAA2026090295583Web · crackedLEFT MLG INBD DOOR WEB APPEARS TO BE CRACKED JUST FWD OF AFT HINGE PAD. PERFORMED HFEC OF SUSPECTED CRACKED. VERIFIED CRACK MEASURES .35IN DOWN INBD SIDE OF WEB AND .20IN ACROSS TOP OF WEB. IAW NDT PART 6 51-00-00, PROCEDURE 23. REMOVED AND SEPERATED INBD &SDR SWAA2026090255517Web · crackedRIGHT MLG INBD DOOR WEB APPEARS TO BE CRACKED JUST FWD OF AFT HINGE PAD. PERFORMED HFEC OF SUSPECTED CRACK. VERIFIED CRACK MEASURES .35IN DOWN INBD SIDE OF WEB AND .20IN DOWN OTBD SIDE OF WEB. REF NDT PART 6 51-00-00 PROCEDURE 23. REMOVED AND SEPERATED INBDSDR SWAA2025120140033Cover · detachedEMERGENCY EXIT SIGN IN THE MID-CABIN FELL OFF CEILING CONNECTION. REINSTALLED EXIT SIGN COVER IAW AMM 33-51-01SDR SWAA2025110626147Handle · looseFORWARD ENTRY DOOR LINING UPPER AND LOWER ASSIST HANDLE ARE LOOSE. TIGHTENED FORWARD ENTRY DOOR LINING UPPER AND LOWER ASSIST HANDLE IAW AMM 52-11-31-400-802 STEP 3.G.(2).SDR SWAA2025110627997Panel · erodedPANEL 193CL L/E WAS WIND ERODED. REPAIRED IAW SRM 51-70-05-2R-6.SDR SWAA2025110625349Attach Angle · crackedCRACK FOUND AT BS 663 VAPOR BARRIER ATTACH ANGLE APPROXIMATELY LBL 9. REPAIRED THE UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5.SDR SWAA2025110625350Attach Angle · crackedCRACK FOUND AT BS 663 VAPOR BARRIER ATTACH ANGLE APPROXIMATELY RBL 9. REPAIRED THE UPPER ATTACH ANGLE IAW SRM 57-10-10-2R-5.SDR SWAA2025081300235Sign · detachedEXIT SIGN MID CABIN FELL OFF DURING DEPLANING. ATTACHED EXIT OVERHEAD SIGN COVER PER AMM 33-51-01 STEP C(4). NO DEFECT FOUND.SDR SWAA2025071189307Flashlight · inoperativeFWD FLIGHT ATTENDANT FLASHLIGHT INOP.SDR SWAA2024121675757Battery Pack · failedEMERGENCY EXIT LIGHT BATTERY PACK M1671 FAILS TO CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1671 IAW AMM 33-51-06-960-805-NG. OPS CHECK GOOD;[02] COMPLETE<BR>AUDIT C/WSDR SWAA2024121675761Battery Pack · failedEMERGENCY EXIT LIGHT BATTERY PACK M1672 FAILS TO CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1672 IAW AMM 33-51-06-960-805;[02] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1672 IAW AMM 33-51-06-960-805. OPS CHECK GOOD;[03] CSDR SWAA2024121675756Battery Pack · failedEMERGENCY EXIT LIGHT BATTERY PACK M1670 FAILS TO CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1670 IAW AMM 33-51-06-960-805; AMM 25-21-46-400-801. OPS CHECK GOOD;[02] COMPLETE<BR>AUDIT C/WSDR SWAA2024121675760Battery Pack · failedEMERGENCY EXIT LIGHT BATTERY PACK M1694 FAILS TO CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1694 IAW AMM 33-51-06-960-805-NG; AMM 25-21-46-400-801.<BR>OPS CHECK GOOD;[02] COMPLETE<BR>AUDIT C/WSDR SWAA2024121675759Battery Pack · failedEMERGENCY EXIT LIGHT BATTERY PACK M1695 FAILS TO CHARGE<[01] OPENED DADO PANEL AT BATTERY PACK M1695 IAW AMM 33-51-06-960-805-NG.<BR><BR>REMOVED & REPLACED BATTERY AT BATTERY PACK M1695 IAW AMM 33-51-06-960-805-NG.<BR><BR>CLOSED DADO PANEL IAW AMM 21-23-03-400SDR SWAA2024121675755Battery Pack · failedEMERGENCY EXIT LIGHT BATTERY PACK M2335 FAILS TO CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M2335 IAW AMM 33-51-06-960-805; AMM 25-21-46-400-801. OPS CHECK GOOD;[02] COMPLETE<BR>AUDIT C/WSDR SWAA2024121675758Battery Pack · failedEMERGENCY EXIT LIGHT BATTERY PACK M1676 FAILS TO CHARGE<[01] REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY PACK M1676 IAW AMM 33-51-06-960-805; AMM 25-21-46-400-801. OPS CHECK GOOD;[02] COMPLETE<BR>AUDIT C/WSDR SWAA2024121672698Circuit Breaker · brokenCIRCUIT BREAKER 'CABIN EMER LIGHTS' ON P6-11 PANEL INBOARD SIDE; BUTTON POOPED OUT AND WILL NOT RESET<[01] REMOVED & REPLACED CABIN EMER LIGHTS CIRCUIT BREAKER A 9 ON P6-11 PANEL IAW SWPM 20-30-00 & 20-83-11<BR>OPS CHECKED CABIN EMER LIGHTS CIRCUIT BREAKER A 9SDR SWAA2024121670417Post · corrodedLAV D; DOOR WILL NOT FULLY CLOSE POSSIBLE CORROSION AT BOTTOM AFT CORNER AT AFT DOOR POST.<[01] REMOVED DOOR POST IAW CMM 25-40-42 REMOVED UPPER FRAME IAW CMM 25-40-42 AND REMOVED TRIM PCS IAW CMM 25-40-42 INSTALLED NEW POST IAW CMM 25-40-42 REINSTALLED ORIGINSDR SWAA2024121669895Floor Panel · pulledFLOOR PANEL 241DF HAS PULLED FIBERS ON UPPER SURFACE.<[01] REFER TO FAULT TTG8Q00X4D6T WHERE EA 24-153-03220 WAS ADDED AS A SUBTASK. REPAIRED FLOOR PANEL 241DF IAW B737 SRM 53-00-50-2R-1.;[02] AUDIT C/WSDR SWAA2024121669898Floor Panel · delaminatedFLOOR PANEL 231XF UPPER SURFACE HAS 2 AREAS OF DELAMINATION.<[01] REFER TO FAULT TTG8Q00X4D6T WHERE EA 24-153-03220 WAS ADDED AS A SUBTASK. REPAIRED FLOOR PANEL 231XF IAW B737 SRM 53-00-50-2R-1.;[02] AUDIT C/WSDR SWAA2024121661030Floor Panel · pulledA177-009 CABIN FLOOR PANEL 221EF HAS PULLING FIBERS ON UPPER SURFACE.<[01] REFER TO FAULT TTG8Q00X4D6T WHERE EA 24-153-03220 WAS ADDED AS A SUBTASK; REPAIRED CABIN FLOOR PANEL IAW SRM 53-00-50-2R-1;[02] AUDIT C/WSDR SWAA2024121661035Floor Panel · delaminatedA177-010 CABIN FLOOR PANEL 231AF HAS DELAMINATION AND PULLING FIBERS ON UPPER SURFACE.<[01] REFER TO FAULT TTG8Q00X4D6T WHERE EA 24-153-03220 WAS ADDED AS A SUBTASK. REPAIRED CABIN FLOOR PANEL 231AF IAW B737 SRM 53-00-50-2R-1.;[02] AUDIT C/WSDR SWAA2024121661031Floor Panel · pulledA177-011 CABIN FLOOR PANEL 231BF HAS MULTIPLE DENTS AND PULLING FIBERS ON UPPER SURFACE.<[01] REFER TO FAULT TTG8Q00X4D6T WHERE EA 24-153-03220 WAS ADDED AS A SUBTASK. REPAIRED CABIN FLOOR PANEL 231BF IAW B737 SRM 53-00-50-2R-1.;[02] AUDIT C/WSDR SWAA2024121661036Floor Panel · pulledA177-012 CABIN FLOOR PANEL 231CF HAS PULLING FIBERS AND A SCRIBE ON UPPER SURFACE.<[01] REFER TO FAULT TTG8Q00X4D6T WHERE EA 24-153-03220 WAS ADDED AS A SUBTASK. CABIN FLOOR PANEL 231CF REPAIRED IAW B737 SRM 53-00-50-2R-1.;[02] AUDIT C/WSDR SWAA2024121661025Floor Panel · pulledA177-001 CABIN FLOOR PANEL 221BF IS BROKEN ON UPPER SURFACE AND HAS FIBERS PULLING.<[01] REPLACED FLOOR PANEL 221BF WITH NEW PART (PART#141A5810-729 BN#492222) PER STANDARD INDUSTRY PRACTICES. FLOOR PANEL WAS INSTALLED ON FAULT #TTG8Q00WA89R<BR>INFO ONLY: A-TASDR SWAA2024121661027Floor Panel · pulledA177-003 CABIN FLOOR PANEL 222BF IS GOUGED ON UPPER SURFACE AND HAS FIBERS PULLING.<[01] REFER TO FAULT TTG8Q00X4D6T WHERE EA 24-153-03220 WAS ADDED AS A SUBTASK. CABIN FLOOR PANEL 222BF REPAIRED IAW SRM 53-00-50-2R-1.;[02] AUDIT C/WSDR SWAA2024121661242Floorbeam · corrodedDOT#12 A-043 CABIN FLOOR STRUCTURE AFT WET AREA 'T' CAP CORRODED AROUND DOMENUT HOLE STA 986 RBL 42 WL 208<[01] 04 - REPAIRED FLOOR BEAM UPPER T CHORD AT STA 986; RBL 42 AND WL 208 PER [SRM 53-70-51-2R-6-B00676 (REPAIR 6 - SECTION 47 - SMALL CORROSION DAMAGE OSDR SWAA2024121661248Structure · corrodedDOT#15 A-043 CABIN FLOOR STRUCTURE AFT WET AREA; 'T' CAP CORRODED AROUND DOMENUT HOLE STA 986 LBL 42 WL 208<[01] CORROSION AT STA 986 LBL 42T CAP AROUND DOMENUT HOLE WAS REMOVED AND REPAIRED I.A.W. SRM 53-70-51-2R-6; ALTERNATIVE 3.;[02] COMPLETE <BR>AUDIT C/W;SDR SWAA2024121661246Structure · corrodedDOT#17 A-043 CABIN FLOOR STRUCTURE AFT WET AREA; CORROSION AROUND LAV MOUNT STA 947 LBL 25 WL 208<[01] 04 - REPAIRED CABIN FLOOR BEAM AT BSTA 947.5 BETWEEN LBL 8 TROUGH LBL 56 AND WL 208 PER [SRM 53-70-51-2R-5-B00675 (REPAIR 5 - SECTION 47 - LARGE CORROSION DASDR SWAA2024121661232Intercostal · corrodedDOT A24-20 AFT PIT RH INTERCOSTAL BETWEEN STATIONS 747 AND 767; RBL 22; WL 156 IS CORRODED ON LOWER SIDE.<[01] REMOVED CORROSION FROM LOWER SIDE OF AFT PIT RH INTERCOSTAL BETWEEN STATIONS 747 AND 767; RBL 22; WL 156 IAW SRM 51-10-02-0G-0; .032' ORIG 'T' .022' SDR SWAA2024121661349Angle · crackedDOT#19 A-043 AFT CARGO COMPARTMENT LEEK ANGLE CRACKED AT STA 867 LBL 11 WL 156<[01] REMOVED CRACKED LEEK ANGLE AT STA 867 LBL 11 WL 156 IN AFT CARGO COMPARTMENT AND REPLACED WITH NEW ANGLE; PN 149A8109-114 ATAG A275021; IAW SRM 51-40-02-0G-0 AND BOEING DWG 149SDR SWAA2024121661243Angle · corrodedDOT#13 A-043 CABIN FLOOR STRUCTURE AFT WET AREA ANGLE CORRODED AROUND 2EA NUTPLATE HOLES STA 986+7' RBL 40 WL 208<[01] REMOVED CORROSION ON ANGLE AROUND 2EA NUTPLATE HOLES STA 986+7' RBL 40 WL 208 I.A.W. 51-10-02-0G-0 ITEM 15 VERIFIED WITH 10X MAGNIFYING GLASSSDR SWAA2024121661233Floor Support · crackedDOT A24-70 MID CABIN FLOOR INTERCOSTAL AT STATION 540 IS CRACKED AT RBL 1.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] C/W REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-BSDR SWAA2024121661234Floor Support · crackedDOT A24-71 MID CABIN FLOOR INTERCOSTAL AT STATION 540 IS CRACKED AT LBL 1.<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)];[02] VERIFIED ITEM 1;[03] C/W REMOVED AND REPLACED PERSDR SWAA2024121661239Floorbeam · corrodedDOT#09 A-043 CABIN FLOOR STRUCTURE AFT WET AREA CORRODED AROUND LAV MOUNT STA 947 RBL 25 WL 208<[01] 01 - REMOVED AND REPLACED INTERCOSTAL LOCATED AT RBL 25 AND WL 208 BETWEEN BSTA 974 TO BSTA 767 PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION SDR SWAA2024121660340Web · corrodedDOT A24-55 AFT PIT RH FORWARD SHIELD I/B SUPPORT WEB CORRODED AROUND NUT PLATES ON LOWER SIDE. STATION 767-787 WL 156 RBL 24.<[01] REMOVE CORROSION ON LOWER SIDE OF AFT PIT RH FORWARD SHIELD I/B SUPPORT WEB STATION 767-787 WL 156 RBL 24 SRM 51-10-02-0G-0; ;050SDR SWAA2024121660490Doubler · missingEGPR DOOR EXISTING REPAIR AT LOWER CUTOUT IS MISSING THE REPAIR FILLER.<[01] FABRICATED AND INSTALLED REPAIR FILLER IAW SRM 53-10-15-2R-4;[02] AUDIT C/WSDR SWAA2024121660074Plate · corrodedAFT CARGO; FWD TIEDOWN PLATE IS CORRODED<[01] REMOVED DAMAGE IAW SRM 53-00-53-1A-1 STEP: 5.B(1)<BR>EVALUATED DAMAGE AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-1 STEP: 5.B(1)<BR>MATERIAL VERIFICATION IAW SRM 53-00-53-1A-1<BR>ATAG: 274044<BR>P/N: 453A2611SDR SWAA2024121660075Structure · corrodedA24-2 AFT PIT FLOOR STRUCTURE STRAP AT DOOR OPENING CORRODED BS 792-847 WL 156 RBL 18<[01] REMOVE CORROSION IAW SRM 51-10-02-0G-0 ITEM 15 AND CHECK WITH 10X MAGNIFYIN GLASS<BR>EVALUATED ALLOWABLE LIMITS 103 ORIG 'T' .084 REMAINING .019 LOSS FOUND OUT OF LIMITSSDR SWAA2024121659685Web · corroded(A125-7) FORWARD CARGO COMPARTMENT; FLOOR STRUCTURE @ DOOR OPENING CORRODED BS440-490; WL156; RBL18-28<[01] 01 - REMOVED AND REPLACED FWD CARGO LOWER MAIN SILL WEB PER [SRM 51-40-02-0G-0-B00069 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENSDR SWAA2024121660076Gusset · crackedDOT A24-77 FWD CARGO COMPARTMENT GUSSET CRACKED AT STA 500I STR 18R<[01] REMOVED AND REPLACED CRACKED GUSSET AT FWD CARGO COMPARTMENT STA 500I 18R IAW RM 51-40-02 BOEING DWG 143A7902 REV B AMM 51-21-91;[02] AUDIT C/WSDR SWAA2024121659681Structure · corroded(A125-1) AFT CARGO COMPARTMENT; FLOOR STRUCTURE @ DOOR OPENING CORRODED BS792-847; WL156; RBL19-28<[01] REMOVED CORROSION AND VERIFIED WITH 10X MAGNIFIER ALL REMOVED IAW SRM 51-10-02-0G-0VERIFIED LIMITS; ORIGINAL THICKNESS .050'; REMAINIG THICKNESS .026'; MATESDR SWAA2024121659678Shield · corroded(A125-3) AFT CARGO COMPARTMENT; FLOOR STRUCTURE; DOOR SHIELD CORRODED BS847-867; WL156; RBL24<[01] 01 - REMOVED AND REPLACED FLOOR STRUCTURE SHIELD ON AFT CARGO COMPARTMENT BETWEEN STA 847 TROUGH STA 867 AT RBL 24 AND WL 156 PER [SRM 51-40-02-0G-0-B00069 (GENESDR SWAA2024121659682Angle · corroded(A125-4) AFT CARGO COMPARTMENT; FLOOR STRUCTURE; Z-ANGLE CORRODED BS727-846; WL156; LBL24<[01] REMOVED; FABRICATED AND REPLACED (INSTALLED) NEW AFT CARGO COMPARTMENT; FLOOR STRUCTURE; Z-ANGLE; WL156; LBL24 WITH EXISTING REPAIR SPLICE AT STA 727J+3' AND 727F-19SDR SWAA2024121659683Angle · corroded(A125-6) AFT CARGO COMPARTMENT; FLOOR STRUCTURE; Z-ANGLE CORRODED BS727-767; WL156; RBL24<[01] REMOVED; FABRICATED AND INSTALLED NEW Z-ANGLE FS 727F-3.5' TO 767; NEW SPLICE LOCATED FS 727F-3.5' WL156; RBL24 AND APPLIED CIC; I.A.W. SRM 51-40-02-0G-0; SRM 53-00-SDR SWAA2024121659668Panel · crackedDOT L7-022: R2 DOOR PANEL 844DZ IS BENT ALOG EDGE OF PANEL AND CRACKED AT RIVET HOLE<[01] REPLACED R-2 DOOR PANEL 844DZ I/W/A SRM 51-40-02-0G-0 A TAG WN48921;[02] VERIFIED ITEM 1<BR>AUDIT C/WSDR SWAA2024121659675Scuff Plate · crackedAFT CARGO DOOR; AFT CORNER SCUFF PLATE IS CRACKED<[01] CRACK ON AFT CARGO DOOR; AFT CORNER SCUFF PLATE WAS REPAIRED ON BACK SHOP W/O 46221/1600/0001 SERIAL NO: 9482708 IAW SRM 53-60-15-2R-1;[02] VERIFIED ITEM 1<BR>AUDIT C/WSDR SWAA2024102149841Lens · unsecureCABIN OVERWING EXIT SIGN SCREW MISSING<[01] REINSTALLED EXIT SIGN LENS PER AMM 33-51-01SDR SWAA2024081325059Door Frame · brokenCA SIDE AFT DOOR FRAME BROKEN<[01] SECURED DOOR FRAME PER SIP
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