# Service difficulty reports: Boeing 767-37D

A list on [Boeing 767-37D](https://openairdocs.org/model/boeing-767-37d.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 7 · 317 reports

- [SDR ABXA20260921415](https://openairdocs.org/sdr/ABXA20260921415.md): Idg · faulted · Sep 21, 2026 · N1327A · Boeing 76737D · Alternator-Generator Drive
  > DURING ENGINE START AND TAXI, L ENG GEN DRIVE & DISC. CREW RETURNED TO THE GATE (BTB). MTC DEFERRED LT ENGINE IDG IAW MEL 24-00-1-1. MBCB 09/24/26. REF ITEM 2, GEN DRIVE LIGHT INOP. MBCB 09/24/26. ACFT REMAINS NO ETOPS. ACFT RETURNED TO SERVICE.
- [SDR ABXA20260816363](https://openairdocs.org/sdr/ABXA20260816363.md): Sense Line · loose · Aug 16, 2026 · N1327A · Boeing 76737D · Pneumatic Distribution System
  > DURING TAXI RT ENG BLEED OFF AND RT PACK OFF EICAS MESSAGE APPEARED A/C RETURNED TO GATE(BTB) AND MTX GROUNDED ACFT AND FOUND PRVC SENSE LINE LOOSE, RESECURED LINE OPS CHECK GOOD IAW AMM 36-11-19 A/C REMAINS ETOPS 180 RETURNED A/C TO SERVICE.
- [SDR ABXA20260814361](https://openairdocs.org/sdr/ABXA20260814361.md): Start Valve · malfunctioned · Aug 14, 2026 · N1327A · Boeing 76737D · Engine Start Valves/Controls
  > DURING TAXI OUT ATTEMPTED TO START NR 1 ENGINE, N2 ADVANCED TO 26% BUT VALVE LIGHT ON L STAYED ILLUMINATED ATTEMPTED 2ND TIME, SAME ISSUE, ACFT RETURNED TO GATE AND MTX GROUNDED ACFT. MTX DEFERRED NR 1 START VALVE IAW MEL 80-00-2-1 FOR DEPARTURE AND RETURNED
- [SDR ABXA20260808356](https://openairdocs.org/sdr/ABXA20260808356.md): A/C Pack · inoperative · Aug 8, 2026 · N1327A · Boeing 76737D · Cabin Cooling System
  > DURING ENGINE START, L PACK INOP. CREW RETURNED TO THE GATE (BTB). MTC RESET L PACK PNUEMATIC SYS IAW AMM 21-00-00 NO DEFECTS NOTED AT THIS TIME L PACK OPERATIONAL A/C REMAINS ETOPS 180. A/C RETURNED TO SERVICE
- [SDR ABXA20260714319](https://openairdocs.org/sdr/ABXA20260714319.md): Starter · inoperative · Jul 14, 2026 · N1327A · Boeing 76737D · Engine Starter
  > DURING TAXI OUT WHILE STARTING RH ENGINE, RH STARTER WAS INOP. A/C RETURNED TO THE GATE (BTB) AND MX GROUNDED A/C. MTX EXERCISED RH START VALVE AND PERFORMED OPS TEST ON ENGINE START VALVE IAW AMM 80-11-00. OPS CHECK GOOD AT THIS TIME. A/C REMAINS ETOPS 180.
- [SDR ABXA20260611254](https://openairdocs.org/sdr/ABXA20260611254.md): Controller · defective · Jun 11, 2026 · N1327A · Boeing 76737D · Pneumatic Distribution System
  > DURING TAXI, CREW RECEIVED R ENG BLEED OFF R PACK OFF NO R DUCT PRESSURE. CREW RETURNED TO THE GATE (BTB). MTX TROUBLE SHOT AND REMOVED AND REPLACED PRV CONTROLLER RH ENGINE IAW B767-300 AMM 36-11-19-004-001-002. OPS CHECK GOOD. PERFORMED RH ENG RUN PER AMM 71
- [SDR ABXA20260516212](https://openairdocs.org/sdr/ABXA20260516212.md): Hinge Arm · failed · May 16, 2026 · N1327A · Boeing 76737D · Passenger Compartment Equipment
  > DURING CREW PREFLIGHT, LEFT UPPER STORAGE BIN DOOR HINGE ARM FAILED. DEFERRED LEFT OVERHEAD STORAGE BIN SHOCK BIN SHOCK STRUT IAW ABX MEL 25-28-1A. DUE TO OVERHEAD BIN STRUT DEFERRAL, PED FIRE BAG DEFERRED IAW ABX NEF 25-03-28. MBCB 5-26-26. PLACARD INSTALLED.
- [SDR ABXA20260429182](https://openairdocs.org/sdr/ABXA20260429182.md): Flap System · faulted · Apr 29, 2026 · N1327A · Boeing 76737D · Trailing Edge Flap Control System
  > DURING DESCENT, LE SLAT DISAGREE LIGHT ILLUMINATED AFTER SELECTING FLAPS 25. CREW EXECUTED A MISSED APPROACH. FOLLOWED QRH PROCEDURES AND LANDED WITH FLAPS 20. MAINTENANCE PERFORMED FSEU READ-OUT FORM IAW AMM ALL SENSORS WITHIN LIMITS. FLAP SLAT SYS OPS NOR
- [SDR ABXA202604264173](https://openairdocs.org/sdr/ABXA202604264173.md): Start Valve · faulted · Apr 24, 2026 · N1327A · Boeing 76737D · Engine Start Valves/Controls
  > DURING TAXI OUT WHILE STARTING NR 1 ENGINE NO ROTATION ON NR 1, START VALVE STAYED OPEN, A/C RETURNED TO THE GATE (BTB) AND MTX GROUNDED A/C AND DEFERRED NR 1 START VALVE IAW MEL ABX-80-00-2-1.A/C REMAINS ETOPS 180. AND RETURNED ACFT TO SERVICE.
- [SDR ABXA20260423171](https://openairdocs.org/sdr/ABXA20260423171.md): Flap System · warning message · Apr 23, 2026 · N1327A · Boeing 76737D · Trailing Edge Flap Control System
  > DURING TAXI, TE FLAP DISAGREE WHEN MOVING TO FLAPS 5 ON THE AFTER START CHECKLIST. CREW RETURNED TO BLOCK (BTB). MTC PERFORMED FIM 27-51 FT 811, RESET BY PASS LEVER. OPS CHECK GOOD. ACFT REMAINS ETOPS 180. ACFT RETURNED TO SERVICE.
- [SDR ABXA20260331142](https://openairdocs.org/sdr/ABXA20260331142.md): Elec Connector · faulted · Mar 31, 2026 · N1327A · Boeing 76737D · Fire Protection System Wiring
  > PILOT REPORTED CARGO FIRE A 4 AMBER INDICATION. RESET ELECTRICAL CONNECTOR. ON BOX. ERROR CLEARED. OPS CHK GOOD. IAW B767 AMM 26-16-00. THIS CLEARS THE DI. PLACARDS REMOVED. NO MAINTENANCE ACTIONS REQUIRED. ACFT REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE
- [SDR ABXA20260313107](https://openairdocs.org/sdr/ABXA20260313107.md): Warning Message · false activation · Mar 13, 2026 · N1327A · Boeing 76737D · Central Display
  > DURING APPROACH INTO MIA, LANDING CONFIG WARNING LIGHT ILLUMINATED AT 3000 FT AGL. FLAPS WERE AT 15 AND GEAR LEVER IN OFF POSITION. CAPTAIN DID A GO AROUND AND CYCLED GEAR. SECOND APPROACH INTO MIA, LANDED WITH NO CONFIG WARNINGS. MAINTENANCE FOUND NO MSG
- [SDR ABXA20260206052](https://openairdocs.org/sdr/ABXA20260206052.md): A/C Pack · inoperative · Feb 6, 2026 · N1327A · Boeing 76737D · Cabin Cooling System
  > DURING TAXI OUT AND AFTER START CHECKLIST, L PACK OFF EICAS DISPLAYED QRH PROCEDURE UNSUCCESSFUL. AIRCRAFT RETURNED TO BLOCKS (BTB). TRANSFERED LH PACK TO DI IAW ABX MEL 21-51-1-1. MX PROCEDURES ACCOMPLISHED PLACARD INSTALLED A/C RELEASED NO ETOPS PLACARD RO
- [SDR ABXA20260116013](https://openairdocs.org/sdr/ABXA20260116013.md): Fire Loop · false indication · Jan 16, 2026 · N1327A · Boeing 76737D · Fire Detection
  > DURING MAINTENANCE INSPECTION, LT ENG OH LP1 EICAS MSG. PLACED ENG OH LP 1 ON DEFERRAL IAW MEL 26-11-2-1 MBCB 01/26/2026 AIRCRAFT ETOPS 120 PLACARD ROTATED. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA20251216342](https://openairdocs.org/sdr/ABXA20251216342.md): Smoke Detector · defective · Dec 16, 2025 · N1327A · Boeing 76737D · Smoke Detection
  > DURING MAINTENANCE INSPECTION, EICAS MSG AFT CARGO DET NR 1 ILLUMINATED. DEFERRED PER MEL 26-16-1-1-1. REMOVED AND REPLACED AFT CARGO SMOKE DETECTOR NR 1 PER AMM 26-16-01. CONFIG 1. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
- [SDR ABXA20250823195](https://openairdocs.org/sdr/ABXA20250823195.md): Support Fitting · corroded · Aug 23, 2025 · N1327A · Boeing 76737D · Horizontal Stabilizer Miscellaneous Structure
  > DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS. #2 FITTINGS TOTAL WERE FOUND TO HAVE CORROSION BETWEEN THE BLADE SEAL AND MATING FLANGE OF THE SUPPORT FITTINGS AND WITHIN THE
- [SDR ABXA20250823194](https://openairdocs.org/sdr/ABXA20250823194.md): Support Fitting · corroded · Aug 23, 2025 · N1327A · Boeing 76737D · Horizontal Stabilizer Miscellaneous Structure
  > DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS. #3 FITTINGS TOTAL WERE FOUND TO HAVE CORROSION BETWEEN THE BLADE SEAL AND MATING FLANGE OF THE SUPPORT FITTINGS AND WITHIN THE
- [SDR ABXA20250823193](https://openairdocs.org/sdr/ABXA20250823193.md): Support Fitting · corroded · Aug 23, 2025 · N1327A · Boeing 76737D · Horizontal Stabilizer Miscellaneous Structure
  > DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS. #4 FITTINGS TOTAL WERE FOUND TO HAVE CORROSION BETWEEN THE BLADE SEAL AND MATING FLANGE OF THE SUPPORT FITTINGS AND WITHIN THE
- [SDR ABXA20250823192](https://openairdocs.org/sdr/ABXA20250823192.md): Support Fitting · corroded · Aug 23, 2025 · N1327A · Boeing 76737D · Horizontal Stabilizer Miscellaneous Structure
  > DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS. #5 FITTINGS TOTAL WERE FOUND TO HAVE CORROSION BETWEEN THE BLADE SEAL AND MATING FLANGE OF THE SUPPORT FITTINGS AND WITHIN THE
- [SDR ABXA20250823191](https://openairdocs.org/sdr/ABXA20250823191.md): Support Fitting · corroded · Aug 23, 2025 · N1327A · Boeing 76737D · Horizontal Stabilizer Miscellaneous Structure
  > DURING THE C-6 MAINTENANCE VISIT AT HAECO GSO, CORROSION WAS FOUND ON THE LH HORIZONTAL STABILIZER LOWER BLADE SEAL SUPPORT FITTINGS.# 6 FITTINGS TOTAL WERE FOUND TO HAVE CORROSION BETWEEN THE BLADE SEAL AND MATING FLANGE OF THE SUPPORT FITTINGS AND WITHIN THE
- [SDR ABXA20250823190](https://openairdocs.org/sdr/ABXA20250823190.md): Support Fitting · corroded · Aug 23, 2025 · N1327A · Boeing 76737D · Horizontal Stabilizer Miscellaneous Structure
  > DURING THE C-6 MAINT VISIT, CORROSION FOUND ON LT HORIZONTAL STAB LOWER BLADE SEAL SUPPORT FITTINGS. NR 7 FITTINGS TOTAL WERE FOUND TO HAVE CORROSION BETWEEN THE BLADE SEAL & MATING FLANGE OF SUPPORT FITTINGS & WITHIN THE SUPPORT ATTACHMENT HOLES. ALL CORROSIO
- [SDR ABXA20250823189](https://openairdocs.org/sdr/ABXA20250823189.md): Skin · damaged · Aug 23, 2025 · N1327A · Boeing 76737D · Fuselage Main, Plate/Skin
  > DURING THE CURRENT C-6 HEAVY MAINTENANCE CHK, MAINT FOUND AT BS 871.5, RT FWD OVERWING EMERG EXIT DOOR HAD NICK DAMAGE ABOVE WINDOW-PLUG CUTOUT. FASTENERS REMOVED AT AFFECTED AREA IAW SRM 51-40-02 & DAMAGE BLENDED OUT IAW SRM 52-20-01 RESULTING IN THE FINAL BL
- [SDR ABXA20250823188](https://openairdocs.org/sdr/ABXA20250823188.md): Panel · damaged · Aug 23, 2025 · N1327A · Boeing 76737D · Nacelle/Pylon, Main Frame
  > DURING THE C-6 MAINTENANCE CHECK, THE NR 2 ENGINE PYLON PANEL ASSEMBLY WAS FOUND TO BE DAMAGED BEYOND REPAIR. MAINTENANCE FABRICATED A NEW PANEL. ACCORDING TO BAC DWG 313T2381 REQUIREMENTS, THE PIECES MUST BE PHOSPHORIC ANODIZED (PAA) AND PRIMED WITH BMS5-13
- [SDR ABXA20250823187](https://openairdocs.org/sdr/ABXA20250823187.md): Door Frame · corroded · Aug 23, 2025 · N1327A · Boeing 76737D · Fuselage Main, Structure
  > DURING C6 CHECK AT HACECO INSPECTION FOUND E&E DOOR CUTOUT FWD FRAME WEB STA303 HAS PUNCTURE REMOVED ANGLE SUPPORT RAIL IAW B767 SRM 51-40-02, REMOVED DAMAGE IAW B767 53-00-07 REPAIR 3. MATL ID FOR FILLER.032 7075 PO1060506.1 AND DOUBLER 7075 T6.040 PO 9837
- [SDR ABXA20250410074](https://openairdocs.org/sdr/ABXA20250410074.md): Tcas System · faulted · Apr 11, 2025 · N1327A · Boeing 76737D · Air Collision Avoidance System
  > DURING PUSHBACK GOT TCAS EICAS MSG. A/C RETURNED TO GATE (BTB) AND MTX GROUNDED A/C, MTX DEFERRED TCAS FOR DEPARTURE IAW MEL ABX-34-45-1A. AND RETURNED A/C TO SERVICE
- [SDR ABX2025F00001](https://openairdocs.org/sdr/ABX2025F00001.md): Autothrottle Sys · warning message · Apr 6, 2025 · N1327A · Boeing 76737D · Auto Throttle System
  > ON TAXI OUT, AUTO THROTTLE DISC LIGHT & AUTO THROTTLE DISC EICAS MESSAGE ILLUMINATED. A/C RETURNED TO BLOCKS (BTB). DEFERRED AUTO THROTTLE IAW MEL ABX-22-30-1. A/C RETURNED TO SERVICE.
- [SDR ABXA20241012187](https://openairdocs.org/sdr/ABXA20241012187.md): Isolation Valve · faulted · Oct 12, 2024 · N1327A · Boeing 76737D · Pneumatic System
  > DURING TAXI R ISLN VALVE LIGHT ON, NO AIR FOR START AC RETURNED TO GATE AND MAITENANCE GROUNDED AC. MTX CYCLED RIGHT ISOLATION VALVE 3 TIMES SUCCESSFULLY PER AMM 36-11-04. AIRCRAFT REMAINS NO ETOPS. RETURNED AC TO SERVICE.
- [SDR ABXA20240919177](https://openairdocs.org/sdr/ABXA20240919177.md): Pressure Switch · faulted · Sep 19, 2024 · N1327A · Boeing 76737D · Hydraulic System, Main
  > AT ROTATION ON TAKEOFF EICAS MSG C HYD SYS PRESS APPEARED AND AC PERFORMED ATB, AND AFTER LANDING MTX GROUNDED AC AND TROUBLE SHOT TO A CTR HYD PRESSURE SWITCH. AND REMOVED AND REPLACED CENTER HYDRALIC SYSTEM PRESSURE SWITCH IAW B767 AMM 29-11-09 OPS CHECK AN
- [SDR UIEA2024031700155](https://openairdocs.org/sdr/UIEA2024031700155.md): Tape · damaged · Mar 18, 2024 · N1327A · Boeing 76737D · Emergency Locator Beacon
  > COCKPIT ELT TAPE DAMAGED. PER MCC REGISTERED WITH NOAA PER ENGINEERING DEPARTMENT IAW AMM 25-63-03. DMI 204893 CLOSED.
- [SDR UIEA2024031700154](https://openairdocs.org/sdr/UIEA2024031700154.md): Elt · unknown · Mar 17, 2024 · N1327A · Boeing 76737D · Emergency Locator Beacon
  > CAPT REPORTED GALLEY ELT NOT TAPED CORRECTLY(<P>R/R GALLEY PORTABLE ELT IAW AMM 25-63-03 PART EFECTIVITY AIPC 25-63-52-97 ITEM 600. NO FURTHER DEFECTS NOTED. THIS CLEARS DMI 204877. </P>)
- [SDR UIEA2024031800156](https://openairdocs.org/sdr/UIEA2024031800156.md): Sign · detached · Mar 17, 2024 · N1327A · Boeing 76737D · Emergency Lighting
  > OBSERVED L1 EMERGENCY EXIT SIGN TO BE DISPLACED(<P>RE-SECURED EMERGENCY EXIT SIGN / LIGHT PER AMM 33-51-01. OPS CHCKS GOOD AT THIS TIME. </P>)
- [SDR UIEA2024010500006](https://openairdocs.org/sdr/UIEA2024010500006.md): Guard · unknown · Jan 5, 2024 · N1327A · Boeing 76737D · Emergency Equipment
  > EMER LIGTHS GUARD SWITCH DOES NOT STAY CLOSED OR SNAPS CLOSED(<P>REMOVED AND REPLACED EMERGENCY LIGHTS GUARD PER AMM 20-11-00 AND 33-51-00-08-01B. OPS CHECKS GOOD. NO FURTHER DEFECTS NOTED </P>)
- [SDR UIEA2023122101009](https://openairdocs.org/sdr/UIEA2023122101009.md): First Aid Kit · unknown · Dec 19, 2023 · N1327A · Boeing 76737D · Emergency Equipment
  > FOUND RED TAG MISSING ON FIRST AID KIT(<P>REMOVED AND REPLACED FIRST AID KIT IAW AMM 25-64-03. NO FURTHER DEFECTS NOTED</P>)
- [SDR UIEA2023100500863](https://openairdocs.org/sdr/UIEA2023100500863.md): Unknown · unknown · Oct 11, 2023 · N1327A · Boeing 76737D · Rudder Structure
  > DELAMINATION ON PREVIOUS REPAIR AT RUD STA 106.142 RUDDER TRAILING EDGE RH.(<P>RUDDER TRAILING EDGE RH AT RUD STA 106.142 WAS REPAIRED IAW SRM 55-40-01-2R-1 FIG. 201 SHEET 2 PAGE 2-3 AND SRM 51-70-04-0G-0 PAR. 5G FIG. 9 SHEET 1 PAGE18,- 38,43 REV.123 AUG 15/20
- [SDR UIEA2023100500864](https://openairdocs.org/sdr/UIEA2023100500864.md): Unknown · unknown · Oct 11, 2023 · N1327A · Boeing 76737D · Fuselage Structure (General)
  > LIGHTNING STRIKE ON FASTENER HEAD AT STA 212.5 AND BELOW RBL 15, UPPER HALF FUSELAGE EXTERIOR.(<P>LIGHTNING STRIKE ON FASTENER HEAD AT STA 212.5 AND BELOW RBL 15, UPPER HALF FUSELAGE EXTERIOR WAS REPAIRED REF SRM 53-00-01-01A-1 AD1, SRM 53-00-01-2R-8 REV 123 1
- [SDR UIEA2023100500865](https://openairdocs.org/sdr/UIEA2023100500865.md): Unknown · unknown · Oct 11, 2023 · N1327A · Boeing 76737D · Fuselage Structure (General)
  > LIGHTNING STRIKE ON FASTENER HEAD AT STA 287 AND 3" BELOW STGR 3 OF UPPER HALF OF FUSELAGE EXTERIOR.(<P>LIGHTNING STRIKE ON FASTENER HEAD AT STA 287 AND 3" BELOW STGR 3 OF UPPER HALF OF FUSELAGE EXTERIOR, WAS REPAIRED REF SRM 53-00-01-1A-1 AD1 FIG 101 TABLE I,
- [SDR UIEA2023100500866](https://openairdocs.org/sdr/UIEA2023100500866.md): Pca · unknown · Oct 11, 2023 · N1327A · Boeing 76737D · Flight Control System
  > OUT OF LIMITS FREE PLAY ON OUTBOARD PCA OF RH ELEVATOR.(<P>OUTBOARD PCA OF RH ELEVATOR WAS REPLACED, ADJUSTED AND LEAK CHECK WAS SATISFACTORY IAW AMM 27-31-05-424-027 REV 139 22APR 2023</P>)
- [SDR UIEA2023100500867](https://openairdocs.org/sdr/UIEA2023100500867.md): Pca · unknown · Oct 11, 2023 · N1327A · Boeing 76737D · Flight Control System
  > OUT OF LIMITS FREE PLAY ON OUTBOARD PCA OF LH ELEVATOR.(<P>N/R: 00028. OUTBOARD PCA OF LH ELEVATOR. WAS REPLACED, ADJUSTED AND TIGHTENED IAW AMM 27-31-05-424-027 & 27-31-00-825-060 REV139 22APR2023</P> / <P> </P> / <P> </P>)
- [SDR UIEA2023100500868](https://openairdocs.org/sdr/UIEA2023100500868.md): Pca · unknown · Oct 11, 2023 · N1327A · Boeing 76737D · Flight Control System
  > OUT OF LIMITS FREE PLAY ON MIDDLE PCA OF LH ELEVATOR.(<P>MIDDLE PCA OF LH ELEVATOR WAS REPLACED, ADJUSTED AND TIGHTENED IAW AMM 27-31-05-424-027 & 27-31-00-825-060 REV 139 22APR2023.</P> / <P> </P>)
- [SDR UIEA2023100500869](https://openairdocs.org/sdr/UIEA2023100500869.md): Hose · unknown · Oct 11, 2023 · N1327A · Boeing 76737D · Detection System
  > FUSELAGE SECTION 43, AREA ABOVE CEILING AT STA 544, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 43, AREA ABOVE CEILING AT STA 544, SMOKE DETECTOR SYSTEM, ORANGE HOSE WAS REPLACED IAW AMM 25-59-01-400-804-001 REV. 139 APR22, 2023.</P>)
- [SDR UIEA2023100500870](https://openairdocs.org/sdr/UIEA2023100500870.md): O-Ring · unknown · Oct 11, 2023 · N1327A · Boeing 76737D · Fuel Storage
  > RH WING OVERWING PORT FUEL LEAK(<P>RH WING OVERWING PORT O-RINGS WERE REPLACED IAW AMM TASK 28-11-04-404-019 REV 140 DATE 22 AUG 23. LEAK TEST WAS PERFORMED, NO LEAKS WERE FOUND</P> / <P> </P>)
- [SDR UIEA2023100500871](https://openairdocs.org/sdr/UIEA2023100500871.md): Hose · unknown · Oct 11, 2023 · N1327A · Boeing 76737D · Fire Protection System
  > FUSELAGE SECTION 43, AREA ABOVE CEILING AT STA 610, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 43, AREA ABOVE CEILING AT STA 610, SMOKE DETECTOR SYSTEM, ORANGE HOSE WAS REPLACED IAW AMM 25-59-01-400-804-001 REV 139 DATE 22 APR 23</P> /
- [SDR UIEA2023100500872](https://openairdocs.org/sdr/UIEA2023100500872.md): Hose · unknown · Oct 11, 2023 · N1327A · Boeing 76737D · Fire Protection System
  > FUSELAGE SECTION 43, AREA ABOVE CEILING BTW STA 654+66 AND STA 654+88, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 43, AREA ABOVE CEILING BTW STA 654:66 AND STA 654:88, SMOKE DETECTOR SYSTEM, ORANGE HOSE WAS REPLACED IAW AMM 25-59-01-40
- [SDR UIEA2023100500873](https://openairdocs.org/sdr/UIEA2023100500873.md): Hose · unknown · Oct 11, 2023 · N1327A · Boeing 76737D · Fire Protection System
  > FUSELAGE SECTION 46, AREA ABOVE CEILING BTW STA 1307 AND STA 1329, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 46, AREA ABOVE CEILING BTW STA 1307 AND STA 1329, SMOKE DETECTOR SYSTEM, ORANGE HOSE WAS REPLACED IAW AMM 25-59-01-400-804-00
- [SDR UIEA2023100500874](https://openairdocs.org/sdr/UIEA2023100500874.md): Hose · unknown · Oct 11, 2023 · N1327A · Boeing 76737D · Fire Protection System
  > FUSELAGE SECTION 46, AREA ABOVE CEILING BTW STA 1461 AND STA 1480, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 46, AREA ABOVE CEILING BTW STA 1461 AND STA 1480, SMOKE DETECTOR SYSTEM, ORANGE HOSE WAS REPLACED IAW AMM 25-59-01-400-804-00
- [SDR UIEA2023100500875](https://openairdocs.org/sdr/UIEA2023100500875.md): Hose · unknown · Oct 11, 2023 · N1327A · Boeing 76737D · Fire Protection System
  > FUSELAGE SECTION 46, AREA ABOVE CEILING AT STA 1395, SMOKE DETECTOR SYSTEM, ORANGE HOSE BROKEN (1EA)(<P>FUSELAGE SECTION 46, AREA ABOVE CEILING AT STA 1395, SMOKE DETECTOR SYSTEM, ORANGE HOSE WAS REPLACED IAW AMM 25-59-01-400-804-001 REV 139 DATE 22 APR 239 AP
- [SDR UIEA2023100500876](https://openairdocs.org/sdr/UIEA2023100500876.md): Computer · unknown · Oct 11, 2023 · N1327A · Boeing 76737D · Elevator Control System
  > STABILIZER TORSION BOX. INTERNAL STRUCTURE, ELEVATOR FUEL COMPUTER BETWEEN STA 1702 AND STA 1725.5. WITH SEVERAL LINES WITH HYD LEAK.(<P>ELEVATOR FEEL COMPUTER WAS REPLACED, TORQUED, CHECKED FOR LEAK, NO LEAK FOUND AND OPERATIONAL TEST WAS SATISFACTORY REF IAW
- [SDR UIEA2023100500877](https://openairdocs.org/sdr/UIEA2023100500877.md): Actuator · unknown · Oct 11, 2023 · N1327A · Boeing 76737D · Elevator Control System
  > STABILIZER TORSION BOX. INTERNAL STRUCTURE BETWEEN STA 1809.5 AND STA 1832, FEEL ACTUATOR WITH EVIDENCE LEAK.(<P>THE FEEL ACTUATOR WAS REPLACED, WAS TIGHTENED AND OPERATIONALTEST WAS SATISFACTORY IAW AMM 27-31-17-424-021 REV140 22AUG2023.</P>)
- [SDR UIEA2023100600878](https://openairdocs.org/sdr/UIEA2023100600878.md): Unknown · unknown · Oct 11, 2023 · N1327A · Boeing 76737D · Fuel Storage
  > FUEL LEAK ON REAR SPAR SPLICE FITTING AND BBR 97.42 AT CENTER TANK.(<P>FUEL LEAK ON REAR SPAR SPLICE FITTING AND BBR 97.42 AT CENTER TANK WAS REPAIRED AND THE TEST WAS SATISFACTORY REF AMM 28-11-00-308-013 REV 140 22AUG23.</P> / <P> </P> / <P> </P>)
- [SDR UIEA2023100600879](https://openairdocs.org/sdr/UIEA2023100600879.md): Angle · unknown · Oct 11, 2023 · N1327A · Boeing 76737D · Fuselage Miscellaneous Structure
  > BULK CARGO COMPARTMENT, FLOOR LEVEL. LH SIDE ANGLE WITH CORROSION AT B.STA 1417 LBL41.(<P> </P> / <P>BULK CARGO COMPARTMENT, FLOOR LEVEL. LH SIDE ANGLE, AT B.STA 1417 LBL41 WAS REPLACED REF SRM 51-10-02-0G-0 PAR.9 REV123 15AUG23.</P> / <P> </P>)

Next page: https://openairdocs.org/model/boeing-767-37d/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 aircraft_model_key = '76737D'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-767-37d/reports

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