# Service difficulty reports: N7740A

A list on [N7740A](https://openairdocs.org/aircraft/N7740A.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 6 · 254 reports

- [SDR SWAA2026051802932](https://openairdocs.org/sdr/SWAA2026051802932.md): Cover · broken · May 14, 2026 · N7740A · Boeing 7377BD · Emergency Lighting
  > FWD ENTRY DOOR EXIT LIGHT NEAR FLOOR LIGHT COVER BROKEN. ACCOMPLISHED INTERIM REPAIR IAW EA M-21-133-00720.
- [SDR SWAA2026031677982](https://openairdocs.org/sdr/SWAA2026031677982.md): Transmitter · erratic · Mar 10, 2026 · N7740A · Boeing 7377BD · Fuel Controlling System
  > NUMBER 2 ENG FUEL FLOW ERRATIC DURING FLIGHT UNTIL ENGINE SHUT DOWN. SOMETIMES BLANKING. ALL OTHER INDICATIONS NORMAL. REMOVED AND REPLACED NR 2 ENG FUEL FLOW TRANSMITTER IAW AMM 73-31-01. LEAK AND OPS CHKD GOOD.
- [SDR SWAA2026022773707](https://openairdocs.org/sdr/SWAA2026022773707.md): Handle · cracked · Feb 24, 2026 · N7740A · Boeing 7377BD · Service Doors
  > PASSENGER CABIN AFT GALLEY SERVICE DOOR HANDLE COVER CRACKED. R & R PASSENGER CABIN AFT GALLEY SERVICE DOOR HANDLE COVER IAW AMM 52-41-31.
- [SDR SWAA2026022673555](https://openairdocs.org/sdr/SWAA2026022673555.md): Door · cracked · Feb 24, 2026 · N7740A · Boeing 7377BD · Landing Gear Doors
  > LEFT MLG CENTER DOOR CRACKED AT FWD SUPPORT ROD FITTING, REMOVED CENTER AND INNER DOOR IAW MM 32-13-11, OK TO CONT REF AUTH 307366. OK TO CONT PER CDL 32-10-3XC SP1B. INSTALLED L/H MLG CENTER DOOR PER AMM 32-13-11.
- [SDR SWAA2026010657828](https://openairdocs.org/sdr/SWAA2026010657828.md): Cover · detached · Jan 3, 2026 · N7740A · Boeing 7377BD · Emergency Lighting
  > FO SIDE EMERGENCY EXIT PLASTIC COVER FELL OFF. REPLACED THE RT OVERWING EXIT EMERGENCY LIGHT ASSEMBLY IAW AMM 33-51 04. OPS CHECKED GOOD.
- [SDR SWAA2025070186298](https://openairdocs.org/sdr/SWAA2025070186298.md): Lamp · inoperative · Jun 28, 2025 · N7740A · Boeing 7377BD · Emergency Lighting
  > R-1 DOOR EXTERIOR EMERGENCY LIGHT INOP. RELAMPED R-1 DOOR EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-04. OPS CHECKED NORMAL.
- [SDR SWAA2025040922421](https://openairdocs.org/sdr/SWAA2025040922421.md): Slide · out of adjust · Apr 7, 2025 · N7740A · Boeing 7377BD · Escape Slide
  > AFT ENTRY DOOR SLIDE NEEDS ADJUSTMENT <[01]. REPLACED AFT ENTRY DOOR SLIDE IAW MT 725-61-06-AE.
- [SDR SWAA2025012287959](https://openairdocs.org/sdr/SWAA2025012287959.md): Seat · misinstalled · Jan 21, 2025 · N7740A · Boeing 7377BD · Passenger Compartment Equipment
  > EXIT ROW SEAT RECLINES; NEED TO LOCK OUT HYDRO-LOCK @ 11 B EXIT ROW SEAT RECLINES NEED TO LOCK OUT HYDRO-LOCK @ 11 B<[01] SECURED EXIT ROW SEAT @ 11B FROM RECLINING IAW CMM 25-21-45.
- [SDR SWAA2025012287966](https://openairdocs.org/sdr/SWAA2025012287966.md): Handle · loose · Jan 21, 2025 · N7740A · Boeing 7377BD · Emergency Exits
  > RT EXIT ROW HANDLE HOUSING IS LOOSE COMING FROM DOOR AND DOOR SHADE @ 12 F<[01] SECURED RT EXIT ROW HANDLE HOUSING COMING FROM DOOR ND DOOR SHADE @12F IAW AMM 52-22-00
- [SDR SWAA2024120272628](https://openairdocs.org/sdr/SWAA2024120272628.md): Slide · loose · Nov 28, 2024 · N7740A · Boeing 7377BD · Escape Slide
  > FWD SERVICE DOOR SLIDE LOCK MECHANISM CAME LOOSE<[01] 02 - INSPECTED PER [AMM 25-66-01-401-NG (DOOR-MOUNTED ESCAPE SYSTEM - REMOVAL/INSTALLATION - PERMANENT)]
- [SDR SWAA2024110154581](https://openairdocs.org/sdr/SWAA2024110154581.md): Power Supply · faulty · Oct 29, 2024 · N7740A · Boeing 7377BD · Emergency Lighting
  > AFT GALLEY FOS SIDE EMERGENCY EXIT LIGHT FLICKERS ON OCCASIONALLY.<[01] PERFORMED OPS CHECK EMERGENCY LIGHTS REF M/M 33-51-00. REMOVED AND REPLACED AFT EMERGENCY EXIT POWER SUPPLY REF M/M 33-51-06.
- [SDR SWAA2024102852698](https://openairdocs.org/sdr/SWAA2024102852698.md): Assist Handle · loose · Oct 24, 2024 · N7740A · Boeing 7377BD · Emergency Equipment
  > LOOSE PAX CABIN FWD ENTRY DOOR AND LEFT BULKHEAD ASSISTANT HANDLES 2024-672814<[01] INSTALLED CORRECTLY FWD ENTRY DOOR AND LEFT BULKHEAD ASSISTANT HANDLES IAW B737-700 AMM 25-21-31-420-802 STEP 3.B ITEM (6) AND AMM 52-11-31-400-802 STEP 3.G ITEM (2);[02] INSTA
- [SDR SWAA2024102852970](https://openairdocs.org/sdr/SWAA2024102852970.md): Assist Handle · loose · Oct 24, 2024 · N7740A · Boeing 7377BD · Emergency Equipment
  > PAX CABIN AFT LEFT AND RIGHT DOORS ASSISTANT HANDLES LOOSE 2024-672824<[01] TIGTHTENED PAX CABIN AFT LEFT AND RIGHT DOORS ASSISTANT HANDLES IAW B737-700 AMM 52-41-31-400-802 STEP 3.F(2) (C) (D) AND B737-700 AMM 52-13-31-400-802 STEP 3.G (2) (C) (D);[02] CERTIF
- [SDR SWAA2024102852812](https://openairdocs.org/sdr/SWAA2024102852812.md): Assist Handle · loose · Oct 24, 2024 · N7740A · Boeing 7377BD · Emergency Equipment
  > PAX CABIN AFT LEFT AND RIGHT DOORS ASSISTANT HANDLES LOOSE 2024-672824<[01] TIGTHTENED PAX CABIN AFT LEFT AND RIGHT DOORS ASSISTANT HANDLES IAW B737-700 AMM 52-41-31-400-802 STEP 3.F(2) (C) (D) AND B737-700 AMM 52-13-31-400-802 STEP 3.G (2) (C) (D);[02] CERTIF
- [SDR SWAA2024102847594](https://openairdocs.org/sdr/SWAA2024102847594.md): Bracket · damaged · Oct 7, 2024 · N7740A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > ALLONGATED HOLE ON BRACKET LOCATE BS663 AND LBL53 AT LEVEL WL210 MAIN WHEEL WELL 2024-589253<[01] REPLACED BRACKET LOCATE BS663 AND LBL53 AT LEVEL WL210 MAIN WHEEL WELL IAW B737-700 SRM 51-10-02 SRM 53-40-51-2R-2 REPAIR 2 SEE INDIVIDUAL SIGNOFF BELOW;[02] REPL
- [SDR SWAA2024102839335](https://openairdocs.org/sdr/SWAA2024102839335.md): Floorbeam · cracked · Sep 19, 2024 · N7740A · Boeing 7377BD · Fuselage Main, Floor Beam
  > CRACK ON BREAK PANEL LOCATED BS 663.7 AND BTW RBL 45.5 AND RBL 60 AT PASSENGER CABIN 2024-589232<[01] REPLACED BREAK PANEL LOCATED BS 663.7 AND BTW RBL 45.5 AND RBL 60 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02; 51-10-02; ITEM 9 AND DWG 144A5701 SHEET 1 REV
- [SDR SWAA2024102839218](https://openairdocs.org/sdr/SWAA2024102839218.md): Floorbeam · cracked · Sep 18, 2024 · N7740A · Boeing 7377BD · Fuselage Main, Floor Beam
  > (CUSTOMER REQUEST) PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75 2024-589223<[01] REPLACED SUPPORT AND FASTENERS LOCATED BS540 BL0 RBL 24.75 IAW B737-700 SRM 51-40-02; B737-700 SRM 51-10-02 AND DRAWING D143A5240-36. SEE INDIV
- [SDR SWAA2024102839213](https://openairdocs.org/sdr/SWAA2024102839213.md): Light · cracked · Sep 18, 2024 · N7740A · Boeing 7377BD · Emergency Lighting
  > CRACK STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT CENTER SECTION (10 EA) 2024-589219<[01] REPLACED STRIP PHOTOLUMINESCENT FLOOR PROXIMITY LIGHTING AT CENTER SECTION PASSENGER CABIN (10 EA) IAW B737-700 AMM 33-51-15-960-801;[02] CERTIFIED TASK COMPLETE <
- [SDR SWAA2024102839214](https://openairdocs.org/sdr/SWAA2024102839214.md): Floorbeam · cracked · Sep 18, 2024 · N7740A · Boeing 7377BD · Fuselage Main, Floor Beam
  > (CUSTOMER REQUEST) PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75 2024-589224<[01] FAULT RESOLVED ON FAULT TTG8Q00VRD6P;[02] FAULT RESOLVED ON FAULT TTG8Q00VRD6P
- [SDR SWAA2024102839026](https://openairdocs.org/sdr/SWAA2024102839026.md): Web · cracked · Sep 18, 2024 · N7740A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK INDICATION (1E/A) FOUND ON HORIZONTAL WEB ON BS 294.5 AT LEVEL STR 17 R FWD GALLEY AREA 2024-589217<[01] REPLACED HORIZONTAL WEB ON BS 294.5 AT LEVEL STR 17 R FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG# 141A8310 SHEET 25 RE
- [SDR SWAA2024102838597](https://openairdocs.org/sdr/SWAA2024102838597.md): Angle · cracked · Sep 17, 2024 · N7740A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATE ON WEB INTERCOSTAL LOCATED BTW BS380 TO BS400 BL0 PASSENGER CABIN 2024-589207<[01] REPLACED ANGLE ON WEB INTERCOSTAL LOCATED BTW BS380 TO BS400 BL0 AT PASSENGER CABIN IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG#143A5400 SHEET 91 REV. - SEE INDI
- [SDR SWAA2024102838085](https://openairdocs.org/sdr/SWAA2024102838085.md): Angle · cracked · Sep 15, 2024 · N7740A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS540 AND RBL 6 AT CENTER WING BOX 2024-589181<[01] REPLACED ANGLE LOCATED BS540 AND RBL 6 AT CENTER WING BOX IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED IAW SRM 51-40-02. CRACK LENGHT IS: 0.5' TOOL USED CALIPER P/N: 500-196-30; S/N: AE2
- [SDR SWAA2024102838086](https://openairdocs.org/sdr/SWAA2024102838086.md): Angle · cracked · Sep 15, 2024 · N7740A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BS 540 AND LBL 6 AT CENTER WING BOX 2024-589179<[01] REPLACED ANGLE LOCATED BS 540 AND LBL 6 AT CENTER WING BOX IAW B737-700 SRM 51-10-02 ITEM 9 AND 51-40-02. CRACK LENGHT IS: 0.753' TOOL USED CALIPER P/N: 500-752-20; S/N: B21014939 AND DUE
- [SDR SWAA2024102837871](https://openairdocs.org/sdr/SWAA2024102837871.md): Angle · cracked · Sep 14, 2024 · N7740A · Boeing 7377BD · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED IRSS 216 AT LT WING 2024-572291<[01] REPLACED ANGLE ON TRAILING EDGE LOCATED IRSS 216 AT LT WING IAW B737-700 SRM 51-10-02; SRM 51-40-02; DWG 115A5552 SHEET 1 REV A SEE INDIVIDUAL SIGN-OFFS BELOW;[02] REPLACED ANGLE ON TRAILIN
- [SDR SWAA2024102837360](https://openairdocs.org/sdr/SWAA2024102837360.md): Skin · cracked · Sep 13, 2024 · N7740A · Boeing 7377BD · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION FOUND ON RT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.600 INCH. APPROX. 2024-572219<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D;
- [SDR SWAA2024102837599](https://openairdocs.org/sdr/SWAA2024102837599.md): Rib · cracked · Sep 13, 2024 · N7740A · Boeing 7377BD · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB LOCATED STAB STA101.90 AND 9 INCHES FROM REAR SPAR AT RT HORIZONTAL STABILIZER 2024-572240<[01] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 210138103; CAL DUE DATE: 10-JUN-25;[02] TOOL USED STEP 6: EDDY CURRENT EQUIPMENT; P/N: NOR
- [SDR SWAA2024102837600](https://openairdocs.org/sdr/SWAA2024102837600.md): Rib · cracked · Sep 13, 2024 · N7740A · Boeing 7377BD · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB LOCATED STAB STA129.50 AND 9 INCHES FROM REAR SPAR LT HORIZONTAL STAB 2024-572241<[01] STEP 3 AND 4 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN:210138503; DUE DATE: 05-AUG-25;[02] REPAIRED INSPAR RIB LOCATED STAB STA129.50 AND 9 INCHE
- [SDR SWAA2024102837596](https://openairdocs.org/sdr/SWAA2024102837596.md): Angle · cracked · Sep 13, 2024 · N7740A · Boeing 7377BD · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED IRSS140 AT RT WING 2024-572231<[01] REPLACED ANGLE TRAILING EDGE LOCATED IRSS140 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND SRM 51-40-02 AND DWG# 115A2000 SHEET 22 REV A. MEASURE OF CRACK IS 1.328? TOOL USED DIGITAL CALIP
- [SDR SWAA2024102837597](https://openairdocs.org/sdr/SWAA2024102837597.md): Plate · cracked · Sep 13, 2024 · N7740A · Boeing 7377BD · Wing Miscellaneous Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 224 AT LT WING 2024-572236<[01] REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED IRSS 224 AT LT WING IAW B737-700 SRM 51-10-02; SRM 51-40-02; DWG # 115A2001 SHEET 136 REV - <BR>SEE INDIVIDUAL SIGN OFF BELOW;[02]
- [SDR SWAA2024102837056](https://openairdocs.org/sdr/SWAA2024102837056.md): Floorbeam · corroded · Sep 12, 2024 · N7740A · Boeing 7377BD · Fuselage Main, Floor Beam
  > CORROSION EXISTING REPAIR ON FLOOR BEAM LOCATED STA 986.5 BTW RBL 44 TO LBL 44 WL 208.1 AT AFT GALLEY AREA 2024-572200<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 200048001; DUE DATE: 28-MAY-25.;[02] TOOL USED: EDDY CURRENT FLAW DETECTO
- [SDR SWAA2024102837059](https://openairdocs.org/sdr/SWAA2024102837059.md): Floorbeam · cracked · Sep 12, 2024 · N7740A · Boeing 7377BD · Fuselage Main, Floor Beam
  > CRACK FLOOR BEAM LOCATED STA294.5 AND RBL52 WL208.1 AT FWD GALLEY AREA 2024-572203<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; P/N P3015GOES00000 S/N 142811019 DUE DATE 23 JAN 25.;[02] TOOL USED RADIOMETER/PHOTOM
- [SDR SWAA2024102837068](https://openairdocs.org/sdr/SWAA2024102837068.md): Intercostal · cracked · Sep 12, 2024 · N7740A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK WEB INTERCOSTAL LOCATED BETWEEN STA294.5 TO STA303.9 AND STR16L AT FWD GALLEY AREA 2024-572212<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; P/N P3015GOES00000 S/N 142811019 DUE DATE 23 JAN 25.;[02] REPAIRED
- [SDR SWAA2024102837069](https://openairdocs.org/sdr/SWAA2024102837069.md): Frame · cracked · Sep 12, 2024 · N7740A · Boeing 7377BD · Fuselage Main, Frame
  > CRACK FRAME LOCATED STA312 AND STR5L TO STR6L AT PASSENGER CABIN 2024-572213<[01] REPAIRED FRAME LOCATED STA312 AND STR5L TO STR6L AT PASSENGER CABIN IAW EA M-22-153-01244.;[02] REPAIRED FRAME LOCATED STA312 AND STR5L TO STR6L AT PASSENGER CABIN IAW EA M-22-15
- [SDR SWAA2024102837359](https://openairdocs.org/sdr/SWAA2024102837359.md): Skin · cracked · Sep 12, 2024 · N7740A · Boeing 7377BD · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.800 INCH. APPROX. 2024-572217<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D;
- [SDR SWAA2024102837060](https://openairdocs.org/sdr/SWAA2024102837060.md): Floor Support · cracked · Sep 12, 2024 · N7740A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA277 TO STA294.5 AND BL0 FWD GALLEY AND LAV 2024-572204<[01] REPLACED WEB-INTERCOSTAL LOCATED BETWEEN STA277 TO STA294.5 AND BL0 FWD GALLEY AND LAV. IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG# 141A5400 S
- [SDR SWAA2024102837062](https://openairdocs.org/sdr/SWAA2024102837062.md): Floor Support · corroded · Sep 12, 2024 · N7740A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA312 TO STA328 AND RBL10 WL208.1 FWD GALLEY AND LAV 2024-572206<[01] REPLACED INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA 312 TO STA 328 AND RBL10 WL208.1 FWD GALLEY AND LAV IAW B737-700 SRM 51-40-02;
- [SDR SWAA2024102837065](https://openairdocs.org/sdr/SWAA2024102837065.md): Structure · cracked · Sep 12, 2024 · N7740A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK INNER CHORD LOCATED STA 303.9 AND LBL 53 AT FWD GALLEY AREA 2024-572208<[01] REPLACED INNER CHORD LOCATED STA 277 TO STA 360 AND LBL 53 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG# 141A8110 SHEET 9 REV. A; DWG#142A0050 SHEET 15 REV. - AND
- [SDR SWAA2024102837067](https://openairdocs.org/sdr/SWAA2024102837067.md): Stringer Clip · cracked · Sep 12, 2024 · N7740A · Boeing 7377BD · Fuselage Main, Attach Fittings
  > CRACK TIE CLIP LOCATED STA277 AND STR10R AT PASSENGER CABIN 2024-572211<[01] REPLACED TIE CLIP AND FASTENERS LOCATED ON STA 277 AND STR 10R AT PASSENGER CABIN IAW B737-700 SRM 51-40-02;AND DWG 141A1110 SHEET 18 REV -;DWG 141A8380 SHEET 14 REV-;SRM 51-10-02; IT
- [SDR SWAA2024102537058](https://openairdocs.org/sdr/SWAA2024102537058.md): Strap · corroded · Sep 12, 2024 · N7740A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION STRAP FLOOR STRUCTURE LOCATED BETWEEN STA1006 TO STA1016 PLUS 25 INCHES AND RBL3 WL208.1 AT AFT GALLEY AREA 2024-572201<[01] REPLACED STRAP AND FASTENERS LOCATED ON FLOOR STRUCTURE BETWEEN STA1006 TO STA1016 PLUS 25 INCHES AND RBL3 WL208.1 AT AFT GAL
- [SDR SWAA2024102537066](https://openairdocs.org/sdr/SWAA2024102537066.md): Stub Frame · cracked · Sep 12, 2024 · N7740A · Boeing 7377BD · Fuselage Main, Frame
  > CRACK STUB FRAME LOCATED STA294.5 AND STR17R AT FWD GALLEY AREA 2024-572210<[01] TOOL USED ON STEP 5 AND 6 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 220272512; CAL DUE DATE: 08-JAN-25;[02] REPAIRED STUB FRAME LOCATED STA294.5 AND STR17R AT FWD GALLEY AREA IAW B737-
- [SDR SWAA2024102437061](https://openairdocs.org/sdr/SWAA2024102437061.md): Floor Support · cracked · Sep 12, 2024 · N7740A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BETWEEN STA312 TO STA328 AND RBL30 FWD GALLEY AND LAV 2024-572205<[01] REPLACED WEB-INTERCOSTAL LOC.BTW STA312 TO STA328 AND RBL30 IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #141A5400 SHEET 39 REV.- SEE INDIVIDUAL
- [SDR SWAA2024102437064](https://openairdocs.org/sdr/SWAA2024102437064.md): Floor Support · cracked · Sep 12, 2024 · N7740A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE BTW STA 344 TO STA 360 AND RBL 33 FWD GALLEY AND LAV 2024-572207<[01] REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE AND FASTENERS BTW STA 344 TO STA 360 AND RBL 33 FWD GALLEY AND LAV IAW B737-700 SRM 51-10-02 ITEM 9 AND INS
- [SDR SWAA2024102836589](https://openairdocs.org/sdr/SWAA2024102836589.md): Stub Frame · cracked · Sep 11, 2024 · N7740A · Boeing 7377BD · Fuselage Main, Frame
  > CRACK INDICATION ON STUB FRAME LOCATED BTW BS 294.5 TO BS 296 AND S-8R TO S-9R AT FWD GALLEY DOOR AREA(1EA). CRACK LENGTH APPROX 1.687 INCH AT PASSENGER CABIN 2024-572141<[01] REPLACED STUB FRAME (1EA) ANGLE (1EA) AND FASTENERS LOCATED BTW BS 294.5 TO BS 296 A
- [SDR SWAA2024102836874](https://openairdocs.org/sdr/SWAA2024102836874.md): Angle · cracked · Sep 11, 2024 · N7740A · Boeing 7377BD · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 273 AT RT WING 2024-572172<[01] REPLACED ANGLE TRAILING EDGE LOCATED AT LEVEL ORSS 273 AT RT WING IAW B737-700 #DWG 115A2930 SHEET: 8 REV:-. AND SRM 51-40-02. AND SRM 51-10-02 ITEM 9.<BR>SEE INDIVIDUAL SIGNS OFF
- [SDR SWAA2024102336436](https://openairdocs.org/sdr/SWAA2024102336436.md): Flashlight · inoperative · Sep 11, 2024 · N7740A · Boeing 7377BD · Emergency Equipment
  > INOP FLASHLIGHT ON WINDSCREEN LT SIDE FWD AREA GALLEY (1EA) 2024-572152<[01] REPLACED FLASHLIGHT ON WINDSCREEN LT SIDE FWD AREA GALLEY (1EA) IAW B737-700 AMM 25-64-00-200-802 STEP10.C(6) AND DWG 25600001 REV H SHEET 4;[02] REPLACED FLASHLIGHT ON WINDSCREEN LT
- [SDR SWAA2024102854220](https://openairdocs.org/sdr/SWAA2024102854220.md): Plate · deteriorated · Sep 10, 2024 · N7740A · Boeing 7377BD · Passenger/Crew Doors
  > DETERIORATED ENTRY DOOR SHIM (2EA) AND ADAPTER PLATE(2EA) GIRT BAR AT AFT GALLEY AREA 2024-572069<[01] REPLACED ENTRY DOOR SHIM (2EA) AND ADAPTER PLATE(2EA) GIRT BAR AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 STEP 3.D(1);[02] COMPLETED
- [SDR SWAA2024102835974](https://openairdocs.org/sdr/SWAA2024102835974.md): Shim · deteriorated · Sep 10, 2024 · N7740A · Boeing 7377BD · Passenger/Crew Doors
  > DETERIORATED ENTRY DOOR SHIM (2EA) AND ADAPTER PLATE(2EA) GIRT BAR AT AFT GALLEY AREA 2024-572069<[01] REPLACED ENTRY DOOR SHIM (2EA) AND ADAPTER PLATE(2EA) GIRT BAR AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 STEP 3.D(1);[02] COMPLETED
- [SDR SWAA2024102854221](https://openairdocs.org/sdr/SWAA2024102854221.md): Plate · deteriorated · Sep 10, 2024 · N7740A · Boeing 7377BD · Service Doors
  > DETERIORATED SERVICE DOOR SHIM (2EA) AND ADAPTER PLATE (2EA) GIRT BAR AT AFT GALLEY AREA 2024-572070<[01] REPLACED SERVICE DOOR SHIM (2EA) AND ADAPTER PLATE (2EA) GIRT BAR AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 STEP 3.D.(1);[02] COMPLETED
- [SDR SWAA2024102835976](https://openairdocs.org/sdr/SWAA2024102835976.md): Girt Bar · deteriorated · Sep 10, 2024 · N7740A · Boeing 7377BD · Emergency Equipment
  > DETERIORATED ENTRY DOOR HARDWARE IN GIRT BAR AT AFT GALLEY AREA 2024-572071<[01] REPLACED ENTRY DOOR HARDWARE IN GIRT BAR AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 STEP 3.D.(1);[02] COMPLETED
- [SDR SWAA2024102835977](https://openairdocs.org/sdr/SWAA2024102835977.md): Girt Bar · deteriorated · Sep 10, 2024 · N7740A · Boeing 7377BD · Emergency Equipment
  > DETERIORATED SERVICE DOOR HARDWARE IN GIRT BAR AT AFT GALLEY AREA 2024-572072<[01] REPLACED SERVICE DOOR HARDWARE IN GIRT BAR AT AFT GALLEY ARE IAW B737-700 AMM 25-66-02-400-801 STEP 3.D.(1);[02] CORRECTED ACTION 1<BR>REPLACED SERVICE DOOR HARDWARE IN GIRT BAR

Next page: https://openairdocs.org/aircraft/N7740A/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 = 'N7740A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7740A/reports

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