# Service difficulty reports: JASC 5700

A list on [JASC 5700](https://openairdocs.org/jasc/5700.md).

Reports filed under 5700 · Wing Structure, newest first.

Page 1 of 49 · 2,401 reports

- [SDR VNAA202610060037](https://openairdocs.org/sdr/VNAA202610060037.md): Hinge Fitting · corroded · Sep 19, 2026 · N648NN · Cndair CL6002D24
  > CORROSION ON HINGE FITTINGS (4 EA`S) WAS FOUND IN THE BONDING JUMPER SETTLEMENT AREA AT RH WING. AREAS ON HINGE FITTINGS (4 EA`S) IN THE BONDING JUMPER SETTLEMENT AREA AT RH WING WERE REPAIRED PER REO 690-57-51-556 REV --.
- [SDR DALA2026082704877](https://openairdocs.org/sdr/DALA2026082704877.md): Structure · cracked · Aug 27, 2026 · N803NW · Airbus A330323
  > A CRACK WAS FOUND AT HOLE 378. REPAIRED PER ERA 636140-14AD. (1779338) AIRCRAFT WAS GROUNDED.
- [SDR CALA2026081918737](https://openairdocs.org/sdr/CALA2026081918737.md): Panel · damaged · Aug 14, 2026 · N37420 · Boeing 737924ER
  > DURING INSPECTION FOUND PANEL 651DB AFT DOOR SUPPORT DAMAGED. REMOVED AND REPLACED WITH NEW SERVICEABLE PANEL ASS REF AMM 57-50-02-400-802.
- [SDR IPXA2026092193152](https://openairdocs.org/sdr/IPXA2026092193152.md): Spar · damaged · Jul 3, 2026 · N144UP · Airbus A300F4622R
  > RIGHT WING TO FUSELAGE UPPER AREA PANEL 677CT LOWER SUPPORT ANGLE HAS (8EA) ELONGTED HOLES. INSTALL NEW SPAR. NEW PART WAS INSTALLED IAW SRM 51-40-21-001.
- [SDR IPXA2026072970144](https://openairdocs.org/sdr/IPXA2026072970144.md): Splice Plate · cracked · Jun 26, 2026 · N583UP · Boeing 7474R7F
  > DURING PERFORM EO-76733-JIC2 STEP 247, FOUND NR 2 FASTENER HOLE CRACK. ACCOMPLISHED REPAIR IAW EO-98163-REQ1 REV.1 AND EGAT EI F2026A57M-1371 REV 3.
- [SDR SWAA2026062913646](https://openairdocs.org/sdr/SWAA2026062913646.md): Fairing · cut · Jun 18, 2026 · N260WN · Boeing 7377H4
  > TWO ELONGATED HOLES ON AFT STRAKE FAIRING AT WINGLET SCIMITAR LT. REPAIRED AFT STRAKE FAIRING AT WINGLET SCIMITAR LT IAW SRM 51-70-04-2R-9 REPAIR 9.
- [SDR IPXA2026061903908](https://openairdocs.org/sdr/IPXA2026061903908.md): Bracket · cracked · Jun 17, 2026 · N334UP · Boeing 76734AF
  > CRACKED BRACKET, RT WING INBD L/E CAVITY TORQUE TUBE SUPPORT BRACKET. INSTALL NEW BRACKET I.A.W SRM 51-40-02-0G REV.95 AND BOEING DWG NO. 114T1240 SH 4 REV: D.
- [SDR REXA2026080401435](https://openairdocs.org/sdr/REXA2026080401435.md): Landing · cracked · Jun 10, 2026 · N146PQ · Cndair CL6002D24
  > SECONDARY NRC FROM TC 900-57-580-503: AFTER REMOVING THE 584FB ACCESS PANEL, ELONGATED HOLE WAS FOUND IN THE SETTLEMENT AREA. SETTLEMENT AREA OF 584FB ACCESS PANEL WAS REPAIRED PER REO 690-57-52-595 REV: - -
- [SDR DALA2026060903438](https://openairdocs.org/sdr/DALA2026060903438.md): Wing · no discrepancy · Jun 2, 2026 · N993AT · Boeing 717200
  > ACFT DUE LT AND RT WING INSPECTIONS AD 2024-21-01. C/W WORKCARDS 5720-01103-01A, AND 5720-01103-01B, FCN'S 95-0557- 8-0032, AND 95-0557-8-0035. OK FOR SVC. (8357674) (AIRCRAFT GROUNDED)
- [SDR KCSA202606021048](https://openairdocs.org/sdr/KCSA202606021048.md): Structure · cracked · Jun 2, 2026 · N712CK · Boeing 7474B5F
  > CRACK IN LOWER T/E STRUCTURE, WS725 JUST AFT OF REAR SPAR
- [SDR IPXA2026051534276](https://openairdocs.org/sdr/IPXA2026051534276.md): Bracket · missing · Apr 16, 2026 · N145UP · Airbus A300F4622R
  > MISSING BRACKET PN: A5796554820500 ON MOVABLE FAIRING 635BB. INSTALLED BRACKET P/N: A57965548205; TRAVELER #: T26/1865162 IN ZONE 600 ON MOVABLE FAIRING 635BB. IAW AIRBUS AIPC 27-51-65-11 ITEM 30, SRM 57-20-35-001 PAG.11 AND SRM 51-40-21-001.
- [SDR KY7A2023FA0000158](https://openairdocs.org/sdr/KY7A2023FA0000158.md): Wing · no discrepancy · Apr 14, 2026 · N832HK · Emb EMB145LR
  > BIRD STRIKE AFTER TAKEOFF, BIRD MADE CONTACT WITH R WING. CLEANED THE REMAINS & PREFORMED BIRD STRIKE INSPECTION IAW FMB145 AMM 05-50-08 NO DAMAGE C\W RTS CHECK
- [SDR SWAA2026051288257](https://openairdocs.org/sdr/SWAA2026051288257.md): Nonskid · deteriorated · Apr 11, 2026 · N8639B · Boeing 7378H4
  > LEFT WING EMERGENCY EXIT WALKWAY REQUIRES TOUCH UP PAINT. APPLIED THE OVERWING EMERGENCY WALKWAY COATING TO LEFT WING EMERGENCY EXIT WALKWAY. IAW AMM 51-21-97-370-802.
- [SDR SWAA2026051288258](https://openairdocs.org/sdr/SWAA2026051288258.md): Nonskid · deteriorated · Apr 11, 2026 · N8639B · Boeing 7378H4
  > RIGHT WING EMERGENCY EXIT WALKWAY REQUIRES TOUCH UP PAINT. APPLIED THE OVERWING EMERGENCY WALKWAY COATING TO RIGHT WING EMERGENCY EXIT WALKWAY. IAW AMM 51-21-97-370-802.
- [SDR IPXA2026050753105](https://openairdocs.org/sdr/IPXA2026050753105.md): Bracket · damaged · Apr 11, 2026 · N141UP · Airbus A300F4622R
  > PANEL 672CB I/B ATTACH FITTING, HOLE ELOGATED 1EA. INSTALLED 2EA.BRACKETS ON PANEL 672CB IAW SRM 51-40 21-001.
- [SDR IXXA2026040901](https://openairdocs.org/sdr/IXXA2026040901.md): Drain Line · dented · Apr 9, 2026 · N227AZ · Boeing 767323
  > LEFT WING SURGE TANK DRAIN LINE IS DENTED AND GOUGED.
- [SDR SWAA2026040784886](https://openairdocs.org/sdr/SWAA2026040784886.md): Nonskid · peeling · Mar 30, 2026 · N8863Q · Boeing 7378
  > RIGHT WING INBD UPPER SURFACE EMERGENCY EXIT NONSLIP WALKWAY HAS AREAS OF PEELING PAINT. TOUCHED UP AREAS OF PEELING PAINT ON THE RIGHT WING I/B UPPER SURFACE EMERGENCY EXIT NONSLIP WALKWAY IAW AMM 51-21-97-370-801.
- [SDR IPXA2026031861571](https://openairdocs.org/sdr/IPXA2026031861571.md): Plate · damaged · Mar 13, 2026 · N162UP · Airbus A300F4622R
  > HOLES IN REINFORCING PLATE P/N: A57244651203 UNDERLYING STRUCTURE LOOKING FWD FOUND HOLE DIAMETER TO BE AT 0.250" 35(EA) WITH SHORT EDGE DISTANCE (1.5D). IT WAS FOUND OUT OF LIMITS. INSTALLED NEW REINFORCING PLATE P/N A57244651203 IAW SRM 51-40-21-001 AND S
- [SDR R61A2026022700052](https://openairdocs.org/sdr/R61A2026022700052.md): Skin · cracked · Feb 27, 2026 · N217JQ · Emb ERJ170200LR
  > WHILE IN HEAVY CHECK - CRACK AT RT WING LOWER SKIN RIB 3A FWD EDGE OF MLG CUTOUT. CUT OUT DAMAGE, FABRICATED, LOCATED AND DRILLED, AND INSTALLED PERMANENT REINFORCING REPAIR REF ETD2026-170-003199.
- [SDR COEA2026032610801](https://openairdocs.org/sdr/COEA2026032610801.md): Access Panel · corroded · Jan 11, 2026 · N801FX · Aerosp ATR72212
  > WO 269490 NR 500039 HEAVY CHECK COE/MAJOR REPAIR: UPPER WING ACCESS PANEL 521DT FOIL FRETTED. LEVEL 2 CORRECTIVE ACTION: REPAIRED PER SRAS DO/TS-4809/07...04337 ISSUE I, DATED 3/2/2026.
- [SDR DALA2025120108775](https://openairdocs.org/sdr/DALA2025120108775.md): None · none · Nov 25, 2025 · N950AT · Boeing 717200
  > SHIP 9509 ER/A 623425-14AD REV C REQUIRES STAGE 2 DTA APRPOVAL. C/W ER/A 623425-14AD. (1321407)
- [SDR CALA2025111711267](https://openairdocs.org/sdr/CALA2025111711267.md): Blowout Panel · detached · Nov 13, 2025 · N77066 · Boeing 767424ER
  > LEFT WING LE SLAT PANEL MISSING SDR FLAGGED NR 5 SLAT OTBD SADDLE BRACKET ATTACHED TO THE BLOWOUT PANEL MISSING ALONG WITH WITH BLOWOUT PANEL. ENGINEERINGS ASSISTANCE REQUESTED. REQUIREMENTS OF ECRA: 5743-02021 CARRIED OUT. NO ADDITIONAL FINDINGS FOUND, LEAK C
- [SDR SWAA2025111333732](https://openairdocs.org/sdr/SWAA2025111333732.md): Rib · cracked · Nov 11, 2025 · N205WN · Boeing 7377H4
  > LEFT WING DEFLECTION CONTROL TAB, RIB CRACKED APPROX 2 FROM AFT EDGE. COMPLETED STEPS UP TO AND INCLUDING STEP 4.P OF LT WING INBD FIXED TE DEFLECTION CONTROL RIB REPAIR IAW SRM 57-51-02-2R-3, REPAIR 3. PERFORMED NDT STEP 4.G PER NDT PART 6 51-00-00 PROCED
- [SDR DALA2025110708136](https://openairdocs.org/sdr/DALA2025110708136.md): Panel · not reported · Nov 2, 2025 · N925AT · Boeing 717200
  > L/H UPPER AFT T/E STRUCTURAL PANEL FROM XF 111.250" TO XTE 206.852". REMOVED L/H UPPER AFT T/E STRUCTURAL PANEL FROM XF 111.250" TO XTE 206.852" (1284968)
- [SDR SWAA2025112028595](https://openairdocs.org/sdr/SWAA2025112028595.md): Paint · degraded · Oct 25, 2025 · N8510E · Boeing 7378H4
  > THE LEFT WING UPPER INBD SURFACE EMERGENCY ESCAPE PATHWAY HAS HEAVILY DEGRADED PAINT. RESTORED FINISH PER AMM 51-21-97-370-802.;[02] INSPECTION C/W
- [SDR F3LA202510230319](https://openairdocs.org/sdr/F3LA202510230319.md): Fitting · corroded · Oct 22, 2025 · N330FR · Airbus A320251N
  > AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION ON RH WING DRY BAY 674AB CORROSION WAS FOUND UNDER MULTIPLE NUTS. INSPECTION AND WORK PERFORMED AS PER EO-A32F-57-32466-01-FINAL. MX ACTION IS ACCEPTABLE.
- [SDR F3LA202510230318](https://openairdocs.org/sdr/F3LA202510230318.md): Fitting · corroded · Oct 22, 2025 · N330FR · Airbus A320251N
  > AIRCRAFT WAS NOT GROUNDED AND IS IN CHECK FOR SCHEDULED MX. DURING INSPECTION ON LH WING DRY BAY 574AB CORROSION WAS FOUND UNDER MULTIPLE NUTS. INSPECTION AND WORK PERFORMED AS PER EO A32F-57-32466-01-FINAL. MX ACTION IS ACCEPTABLE.
- [SDR VNAA2025F00020](https://openairdocs.org/sdr/VNAA2025F00020.md): Support · corroded · Oct 14, 2025 · N501BG · Cndair CL6002C10
  > DISCREPANCY: THE LANDING FOR PANEL 642ET IS CORRODED. CORRECTIVE ACTION: REPAIRED LANDING IAW MHIRJ REO 670-57-21-1032 REV-- DATED 2025-1-13
- [SDR AALA202510295385](https://openairdocs.org/sdr/AALA202510295385.md): Rod · excess play · Oct 3, 2025 · N865NN · Boeing 737823
  > AIRCRAFT WAS NOT GROUNDED: LEFT WING, BETWEEN SPOILER NUMBER 5 AND 6, AFT OF AFT SPAR, INBOARD SIDE BOTH RODS HAVE EXCESSIVE PLAY. REMOVED AND REPLACED BEAM ASSEMBLY AT LEFT WING. PER B737NG SRM 51-40-02, SRM 51-40-05, SRM 51-20-01.
- [SDR DALA2025100807327](https://openairdocs.org/sdr/DALA2025100807327.md): Sealant · not reported · Oct 2, 2025 · N981AT · Boeing 717200
  > WORKING ERA 629612-14AD REV ORIG STEPS 18-20 NEED TO BE ACCOMPLISHED. C/W STEP 18 OF ERA 629612-14AD REV ORIG, RESTORED SEALANT REMOVED FOR INSPECTIONS PER B717 51-24-00 & DWG'S. C/W STEP 19 OF ERA 629612-14AD (1239562)
- [SDR DALA2025092406976](https://openairdocs.org/sdr/DALA2025092406976.md): Limiter · damaged · Sep 23, 2025 · N994AT · Boeing 717200
  > ON WAKEUP FOUND SPEED TAPE ON RH VORTILON. DAMAGE WITHIN LIMITER PER EAA 570743-14MA REV B APPLIED TEMP REPAIR. WILL NEED PERMINENT REPAIR WITHIN 100 FLIGHT HOURS.(7372557)
- [SDR SWAA2025100213158](https://openairdocs.org/sdr/SWAA2025100213158.md): Paint · peeling · Sep 9, 2025 · N7833A · Boeing 73779P
  > CORROSION SUPPORT STRUCTURE ACCESS PANEL 551FB TRAILING EDGE AT LT WING. PERFORMED DETAIL VISUAL INSPECTION ON SUPPORT STRUCTURE ACCESS PANEL 551FB TRAILING EDGE AT LT WING AND NO CORROSION FOUND, ONLY PEELING PAINT IAW SRM 51-10-02. NO MAINTENANCE ACTION IF
- [SDR SWIA2025120200903](https://openairdocs.org/sdr/SWIA2025120200903.md): Guide · worn · Sep 3, 2025 · N897SK · Cndair CL6002D24
  > DURING AAI AUDIT OF 2C TASK CARD 57-690-304, FOUND THE LT SIDE ROLLER GUIDE IS SHOWING SIGNS OF WEAR. COMPLIED WITH THE REPAIR OF THE LT SIDE ROLLER GUIDE IAW REO 690-57-51-467, REV -. OPS CHECK GOOD.
- [SDR CALA2025082708186](https://openairdocs.org/sdr/CALA2025082708186.md): Tape · unsecure · Aug 24, 2025 · N892UA · Airbus A319132
  > FA REPORTS ABNORMALLY LO UD WHISTLE FROM RIGHT OV ERWING EXIT. SECURED LOOSE TAPE ON RIGHT WING.
- [SDR FDEA202508181494](https://openairdocs.org/sdr/FDEA202508181494.md): Repair · not reported · Aug 18, 2025 · N522FE · Doug MD11F
  > EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER BETWEEN STATION XOS 621 TO XOS 625 EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT BEADED DOUBLER BETWEEN STATION XOS 621 TO XOS 625 EVALUATED AND FOUND REPAIR
- [SDR DALA2025080505856](https://openairdocs.org/sdr/DALA2025080505856.md): Strut · loose · Aug 3, 2025 · N346NB · Airbus A319114
  > LEFT WING INTERCONNECTING STRUT LOOSE. CORRECTIVE ACTION: REPLACED BEARING AT LH WING I/B FLAP INTERCONNECTING SUPPORT STRUT ATTACH FITTING IAW A319 CMM TASK 57-52-21-300-803-A01. (1122721).
- [SDR DALA2025080505855](https://openairdocs.org/sdr/DALA2025080505855.md): Strut · loose · Aug 3, 2025 · N346NB · Airbus A319114
  > RIGHT WING INTERCONNECTING STRUT WITH LOOSENESS. CORRECTIVE ACTION: REPLACED BEARING AT RH WING I/B FLAP INTERCONNECTING SUPPORT STRUT ATTACH PAINT IAW A319 CMM TASK 57-52-21-300-803-A01. (1122710).
- [SDR FDEA202506140936](https://openairdocs.org/sdr/FDEA202506140936.md): None · none · Jun 14, 2025 · N525FE · Doug MD11F
  > AGING AIRCRAFT - EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT RIB DOUBLER STATION XOS 789.645 (REPLACED DOUBLER P/N ARB3954-8 BY FABRICATION) EXISTING REPAIR AT RIGHT HAND WING FIXED LEADING EDGE COMPARTMENT RIB DOUBLER STATION XOS 789
- [SDR FDEA202506140935](https://openairdocs.org/sdr/FDEA202506140935.md): None · none · Jun 14, 2025 · N525FE · Doug MD11F
  > AGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT RIB DOUBLER STATION XOS 789.645 (REPLACED DOUBLER P/N ARB3954-7 BY FABRICATION) EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE COMPARTMENT RIB DOUBLER STATION XOS 789.6
- [SDR FDEA202506140934](https://openairdocs.org/sdr/FDEA202506140934.md): None · none · Jun 14, 2025 · N525FE · Doug MD11F
  > AGING AIRCRAFT - EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE LOWER STRINGER DOUBLER STATION XOS 906.5607 EXISTING REPAIR AT LEFT HAND WING FIXED LEADING EDGE LOWER STRINGER DOUBLER STATION XOS 906.5607 EVALUATED AND FOUND REPAIRED IAW MD11 SRM 5
- [SDR SWAA2025072180824](https://openairdocs.org/sdr/SWAA2025072180824.md): Access Panel · damaged · Jun 12, 2025 · N294WN · Boeing 7377H4
  > ELONGATED HOLES ON ACCESS PANEL 661CB. REPAIRED ACCESS PANEL 661CB IAW B737-700 SRM 51-70-04-2R-10 REPAIR 10.
- [SDR UIEA2025060200713](https://openairdocs.org/sdr/UIEA2025060200713.md): Structure · damaged · Jun 11, 2025 · N499MC · Boeing 74747UF
  > LHW O/B MID FLAP FOUND BOLT HOLE ELONGATED.(<P>PERFORMED REPAIR AT ELONGATED BOLT HOLE AS PER SRM 51-70-07 PAR 5.K REV 103. NO FURTHER DEFECTS NOTED.</P>)
- [SDR DALA2025060604324](https://openairdocs.org/sdr/DALA2025060604324.md): Repair · not reported · May 25, 2025 · N949AT · Boeing 717200
  > SHIP 9500 EXISTING REPAIR FOUND PER ERA 623617-14AD REV ORIG. CORRECTIVE ACTION: REPAIRED PER 623617-14AD (0986223)
- [SDR DALA2025051503762](https://openairdocs.org/sdr/DALA2025051503762.md): Not Reported · damaged · May 13, 2025 · N3763D · Boeing 737832
  > (LOG 0963092) PERFORM PERMANENT REPAIR IN ACCORDANCE SRM 57-10-10-2R PROCEDURE 3. PERMANENT REPAIR IN ACCORDANCE B737-800 SRM 57-10-10-2R PROCEDURE 3, REPAIR 3 ALTERNATIVE 2 WAS PERFORMED.
- [SDR 9WGA2025070154519](https://openairdocs.org/sdr/9WGA2025070154519.md): Support · cracked · May 2, 2025 · N545JN · Doug MD11F
  > DURING HEAVY MAINTENANCE LH FLAP HINGE SUPPORT WAS FOUND CRACKED.
- [SDR DALA2025043003315](https://openairdocs.org/sdr/DALA2025043003315.md): Repair · not reported · Apr 29, 2025 · N986AT · Boeing 717200
  > -AD- EXISTING REPAIR FOUND, CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURE PRIOR TO FURTHUR FLIGHT REF. FC5720-01103. AMOC 24-160 TO AD 2024-21-01 PARA(G) W/C 5720-01103-01B AND ERA 621136-14AD REV ORIGINAL ALREADY APPROVED AND PROVIDE AMOC TO SUBJECT AD FOR
- [SDR DALA2025043003314](https://openairdocs.org/sdr/DALA2025043003314.md): Repair · not reported · Apr 28, 2025 · N980AT · Boeing 717200
  > -AD- EXISTING REPAIR FOUND, OK TO CONT THE WC INSP AS AUTHORIZED BY THE TIME CONT ITEMS STATEMENT FOR SEC I OF ERA 619064-14AD REV B. (LP #7184929)
- [SDR UIEA2025042100557](https://openairdocs.org/sdr/UIEA2025042100557.md): Fastener · not reported · Apr 22, 2025 · N5113A · Boeing 73783N
  > WINGS - WING LEADING EDGE - UPPER SKIN PANEL - FASTENER CHANGE - SB 737-57-1336 R0 IAW PAR-B1920 REV.0.(<P>REPLACED FASTENER IAW ATLAS AIR PAR-B REV 0 DATED: 17JAN25 AND BOEING 737-800 BCF SRM 57-41-01-2R-7 REPAIR 7 PARG 4 TABLE 201 FIG 202, REV 23 DATED: 10MA
- [SDR CALA2025042104037](https://openairdocs.org/sdr/CALA2025042104037.md): Wing · smoke · Apr 19, 2025 · N484UA · Airbus A320232
  > RAMP REPORTS SMOKE COMING FROM WINGS, BURNING SMELL. CONTACTED FIRE DEPARTMENT, NO HEAT SHOWN ON THERMAL IMAGING, NO BURNING SMELL, NO EVIDENCE OF HEAT DAMAGE FOUND. DROPPED FLAP/S SLATS ON GROUND REF AMM 27-50-00, INSPECTED, SMOKE APPEARS TO CONDENSATION WI
- [SDR VNAA20250528001](https://openairdocs.org/sdr/VNAA20250528001.md): Hinge Fitting · gouged · Apr 18, 2025 · N553NN · Bombdr CL6002D15
  > RH WING SPS21.80 OUTBOARD HINGE FITTING GOUGE. RH WING SPS21.80 OUTBOARD HINGE FITTING GOUGE WAS REPAIRED PER REO 690-57-51-421 REV --.

Next page: https://openairdocs.org/jasc/5700/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 jasc_code = '5700'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5700/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.