# Service difficulty reports: N7737E

A list on [N7737E](https://openairdocs.org/aircraft/N7737E.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 5 · 217 reports

- [SDR SWAA2025100821659](https://openairdocs.org/sdr/SWAA2025100821659.md): Lamp · inoperative · Oct 6, 2025 · N7737E · Boeing 7377BD · Emergency Lighting
  > EMERGENCY LIGHT AT SEAT ROW 19DEF INOPERATIVE. REPLACED THE LAMP EMERGENCY LIGHT AREA LIGHT AT 19DEF PER AMM 33-51-03.
- [SDR SWAA2025061280284](https://openairdocs.org/sdr/SWAA2025061280284.md): Seat Back · out of adjust · Jun 11, 2025 · N7737E · Boeing 7377BD · Passenger Compartment Equipment
  > SEAT 11B (IN EMERGENCY EXIT ROW) RECLINES.<[01] C/W;[02] ADJUSTED HYDRO-LOCKS TO THE LOCKED POSITION PER AMM 25-22-00
- [SDR SWAA2025061280564](https://openairdocs.org/sdr/SWAA2025061280564.md): Lamp · inoperative · Jun 11, 2025 · N7737E · Boeing 7377BD · Emergency Lighting
  > RIGHT EMERGENCY EXIT OVERHEAD LIGHT IS INOP.<[01] RELAMPED PER AMM 33-51-01;[02] VERIFIED RELAMPED PER AMM 33-51-01
- [SDR SWAA2025061180289](https://openairdocs.org/sdr/SWAA2025061180289.md): Scuff Plate · cracked · Jun 11, 2025 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > FORWARD CARGO THRESHOLD BULLNOSE IS SPLIT; CRACKED.<[01] 01 - REMOVED AND REPLACED PER [AMM 53-11-02-401-NG (CARGO DOOR SCUFF PLATE - REMOVAL/INSTALLATION - PERMANENT)];[02] VERIFIED REMOVED AND REPLACED PER AMM 53-11-02-401-NG CARGO DOOR SCUFF PLATE.
- [SDR SWAA2025012288226](https://openairdocs.org/sdr/SWAA2025012288226.md): Girt Bar · out of position · Jan 22, 2025 · N7737E · Boeing 7377BD · Emergency Equipment
  > R1 DOOR ESCAPE SLIDE GIRT REQUIRES REPACK.<[01] REPACKED R1 DOOR ESCAPE SLIDE GIRT PER MT257-61-06 AND AMM 25-66-01
- [SDR SWAA2024091236467](https://openairdocs.org/sdr/SWAA2024091236467.md): Lamp · inoperative · Sep 11, 2024 · N7737E · Boeing 7377BD · Emergency Lighting
  > R2 DOOR EMERGENCY LIGHT INOP. RELAMPED R2 DOOR EMERGENCY LIGHT PER AMM 33-51-04-960-801.
- [SDR SWAA2024090331237](https://openairdocs.org/sdr/SWAA2024090331237.md): Seal · cracked · Aug 28, 2024 · N7737E · Boeing 7377BD · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDER CRACKED.<[01] REMOVED AND REPLACED RIGHT HORIZONTAL STABILIZER UPPER FORWARD SLIDING SEAL PER AMM 53-31-31.
- [SDR SWAA2024083031236](https://openairdocs.org/sdr/SWAA2024083031236.md): Slide · out of position · Aug 28, 2024 · N7737E · Boeing 7377BD · Escape Slide
  > R2 GALLEY DOOR SLIDE LOWER FLAP REQUIRES REPOSITION.<[01] REPOSITIONED ESCAPE SLIDE LOWER FLAP PER AMM 25-66-01 R2 DOOR
- [SDR SWAA2024072214639](https://openairdocs.org/sdr/SWAA2024072214639.md): Power Supply · faulty · Jul 19, 2024 · N7737E · Boeing 7377BD · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ARC HALF ON HALF OFF WITH AIRCRAFT ON GROUND POWER ON APU POWER.<[01] R/R RIGHT AFT POWER SUPPLY AS PER AMM 33-51-06. OPS CK OK. NO FAULTS NOTED AT THIS TIME.
- [SDR SWAA2024071512491](https://openairdocs.org/sdr/SWAA2024071512491.md): Adiru · unreliable · Jul 14, 2024 · N7737E · Boeing 7377BD · Attitude Gyro and Indicating System
  > CREW REPORTS F/O LOST FLIGHT DISPLAY; AIRSPEED UNRELIABLE AND MACH A/S WARNING CONTINUOUS.<[01] R/R #2 ADIRU PER AMM 34-21-01. OPS CHECK GOOD. AIRCRAFT RECERTIFIED TO CATIII STATUS PER MT 734-00-03 VER# 42689
- [SDR SWAA2024071108301](https://openairdocs.org/sdr/SWAA2024071108301.md): Battery Pack · inoperative · Jul 3, 2024 · N7737E · Boeing 7377BD · Emergency Lighting
  > ALL EMERGENCY LIGHTS ASSOCIATED WITH EMERGENCY EXIT LIGHT BATTERY PACKS M1669 AND M1668 ARE INOP<[01] REMOVED AND REPLACED BOTH BATTERY PACKS M1669 AND M1668; PERFORMED A GOOD TEST PER AMM 33-51-06-960-805;[02] UPDATED STEP TO FINAL;[03] VERIFIED UPDATES;[04]
- [SDR SWAA2024071106961](https://openairdocs.org/sdr/SWAA2024071106961.md): Lens · broken · Jun 28, 2024 · N7737E · Boeing 7377BD · Emergency Lighting
  > G4 GALLEY EMERGENCY LIGHT LENS BROKEN<[01] REMOVED AND REPLACED G4 GALLEY EMERGENCY LIGHT LENS PER AMM 33-51-01-960-802.;[02] VERIFIED REPLACEMENT OF G4 GALLEY EMERGENCY LIGHT LENS
- [SDR SWAA2024071106062](https://openairdocs.org/sdr/SWAA2024071106062.md): Connector · damaged · Jun 26, 2024 · N7737E · Boeing 7377BD · Light System Wiring
  > G4 GALLEY LOWER EMERGENCY EXIT LIGHT HAS DAMAGED CONNECTORS.<[01] REPLACED CONNECTORS FOR G4 GALLEY LOWER EMERGENCY EXIT LIGHT AND PERFORMED GOOD OPERATIONAL CHECK IAW SWPM 20-30-12 AND AMM 33-51-00-710-801.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024071105682](https://openairdocs.org/sdr/SWAA2024071105682.md): Lens · broken · Jun 25, 2024 · N7737E · Boeing 7377BD · Emergency Lighting
  > FWD LAV 'A' EMERGENCY EXIT LIGHT LENS BROKEN<[01] REMOVED AND REPLACED FWD LAV 'A' EMERGENCY EXIT LIGHT LENS PER AMM 33-51-01-960-802.;[02] VERIFIED FWD LAV 'A' EMERGENCY EXIT LIGHT LENS REPLACEMENT
- [SDR SWAA2024071100096](https://openairdocs.org/sdr/SWAA2024071100096.md): Attach Angle · cracked · Jun 10, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > L/H BS663 UPPER ATTACH ANGLE IS CRACKED ON VAPOR BARRIER LBL8 WL167.68<[01] CORRECTION ON STEPS 8 AND 10 (ITEMS 3;4) REFERENCE SHOULD BE SRM 57-10-10-2R-5 REPAIR 5 INSTEAD OF SRM 51-10-10-2R-5 REPAIR 5.;[02] CRACK ON L/H BS 663 UPPER ATTACH ANGLE LBL8 WL167.68
- [SDR SWAA2024071198551](https://openairdocs.org/sdr/SWAA2024071198551.md): Seat Track · corroded · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RH SEAT TRACK BS 559+ 3 WELL; 597-5 WELL; 685-3 CROWN; 685-6 WELL; 694 CROWN; 694 WELL; 706-3 WELL; 727-3 WELL; 727A+8 WELL; 727A+8 CROWN; RBL 45; WL 208.<[01] COMPLETED STEPS 1-10 AND PARTIAL STEP 11.;[02] COMPLETED STEP 12;[03] UPDATED STEP 11;[
- [SDR SWAA2024071198731](https://openairdocs.org/sdr/SWAA2024071198731.md): Floorbeam · corroded · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM BS 986 BL0-RBL 43 AND LBL 43 WL 208.<[01] REMOVED AND REPAIRED DAMAGE UPPER FLANGES OF THE BS986 T-CHORD LBL50-RBL50 I.A.W SRM 53-70-51-2R-4 REPAIR 4; EA-M-24-153-01563-WIP1 CCN TTG8Q00TV85G AND BOEING DWGS 147A5600;147A0000;147A8501 A
- [SDR SWAA2024071198734](https://openairdocs.org/sdr/SWAA2024071198734.md): Shear Web · corroded · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON R/H AFT SHEAR WEB BS 1016-1029 BL0-RBL 14 WL 208.<[01] REMOVED AND REPLACED R/H SHEAR WEB BS 1016-1029 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5600;[02] TASK COMPLETED;[03] VERIFIED COMPLETE STEP 4; CARD COMPLETE.
- [SDR SWAA2024071198727](https://openairdocs.org/sdr/SWAA2024071198727.md): Shear Web · corroded · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON L/H AFT SHEAR WEB BS 1016-1026 BL0-LBL 12 WL 208.<[01] REMOVED AND REPLACED SHEAR WEB BS 1016-1029 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5600;[02] VERIFIED COMPLETE STEP 7; CARD COMPLETE.
- [SDR SWAA2024071198735](https://openairdocs.org/sdr/SWAA2024071198735.md): Strap · corroded · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON REINFORCEMENT STRAP BS 1027 RBL 17 WL 208.<[01] COMPLETED STEPS 1 & 3.;[02] REMOVED AND REPLACED A NEW TENSION STRAP BS1006-BS1027 RBL 17 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5600 SH 46.;[03] VERIFIED ACTION 1.;[04] JOB COMPLETE.
- [SDR SWAA2024071198728](https://openairdocs.org/sdr/SWAA2024071198728.md): Strap · corroded · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON REINFORCEMENT STRAP BS 1018-1027 RBL 2.5 WL 208.<[01] COMPLETED STEPS 1 AND 3.;[02] REMOVED AND REPLACED A NEW TENSION STRAP BS1006-BS1027 RBL 3 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5600 SH 46;[03] VERIFIED ACTION 1.;[04] JOB COMPLETE.
- [SDR SWAA2024071198729](https://openairdocs.org/sdr/SWAA2024071198729.md): Strap · corroded · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON REINFORCEMENT STRAP BS 1023 LBL 3.5 WL 208.<[01] REMOVED AND REPLACED A NEW TENSION STRAP BS1006-BS1027 LBL 3.5 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5600 SH 44.;[02] VERIFIED ACTION 1.<BR>JOB COMPLETE.
- [SDR SWAA2024071198730](https://openairdocs.org/sdr/SWAA2024071198730.md): Strap · corroded · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION ON REINFORCEMENT STRAP BS 1025-1028 LBL 17.5 WL 208.<[01] OK TO INSTALL STRAP.;[02] REMOVED AND REPLACED A NEW TENSION STRAP BS1006-BS1027 LBL 17.5 WL208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 147A5600 SH44.;[03] VERIFIED ACTION 2.<BR>JOB COMPLETE.
- [SDR SWAA2024071098722](https://openairdocs.org/sdr/SWAA2024071098722.md): Intercostal · cracked · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 380-400 RBL 8 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL BS 380-400 RBL 8 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 143A5400;[02] VERIFIED COMPLETE
- [SDR SWAA2024071098721](https://openairdocs.org/sdr/SWAA2024071098721.md): Intercostal · cracked · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 380-400 LBL 14 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL BS 380-400 LBL 14 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 143A5400
- [SDR SWAA2024071098720](https://openairdocs.org/sdr/SWAA2024071098720.md): Intercostal · cracked · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 380-400 LBL 1 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 380-400 LBL1 WL 208. I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 143A5400;[02] VERIFIED
- [SDR SWAA2024071098719](https://openairdocs.org/sdr/SWAA2024071098719.md): Intercostal · cracked · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 380-400 RBL 41 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL BS 380-400 RBL 41 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 143A5400
- [SDR SWAA2024071098713](https://openairdocs.org/sdr/SWAA2024071098713.md): Intercostal · cracked · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 328-344 LBL 46 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL BS328-BS344 LBL46 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DOCUMENT 141A5400 DWG ID:0044.;[02] VERIFIED COMPLETE;[03] VERIFIED COMPLETE
- [SDR SWAA2024071098718](https://openairdocs.org/sdr/SWAA2024071098718.md): Intercostal · cracked · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 312-328 LBL 44 WL 208.<[01] INSTALLED NEW INTERCOSTAL BS 312-328 LBL 44 WL 208 I.A.W. SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPS 1-3.
- [SDR SWAA2024071098717](https://openairdocs.org/sdr/SWAA2024071098717.md): Floor Support · cracked · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 312-328 RBL 31 WL 208.<[01] INSTALLED INTERCOSTAL BS 312-328 RBL 31 WL 208 SRM 51-40-02-0G-0;[02] VERIFIED CORRECTIVE ACTION ENTRY 1. WITH STEPS 1-3.
- [SDR SWAA2024071098716](https://openairdocs.org/sdr/SWAA2024071098716.md): Floor Support · cracked · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED INTERCOSTAL BS 277-294 RBL 1 WL 208.<[01] REMOVED AND REPLACED INTERCOSTAL BS 277-294 RBL 1 WL 208 I.A.W SRM 51-40-02-0G-0 AND BOEING DWG 141A5400
- [SDR SWAA2024071098715](https://openairdocs.org/sdr/SWAA2024071098715.md): Angle · cracked · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACKED ANGLE BS 294 RBL 55 WL 208.<[01] UPDATED STEPS 4 AND 5.;[02] REMOVED DAMAGE ANGLE AND INSTALLED REPAIR ANGLE BS291-294.5 RBL55 WL 208 IAW SRM 53-10-15-2R-7.;[03] VERIFIED COMPLETE
- [SDR SWAA2024071098714](https://openairdocs.org/sdr/SWAA2024071098714.md): Floorbeam · cracked · Jun 5, 2024 · N7737E · Boeing 7377BD · Fuselage Main, Floor Beam
  > CRACKED FLOOR BEAM BS 294 RBL 53 WL 208.<[01] REMOVED DAMAGED SECTION OF UPPER CHORD; REPLACED WITH NEW SECTION OF UPPER CHORD AND INSTALLED REPAIR PARTS AT BS294.5 RBL15-RBL59 WL208 IAW SRM 53-10-51-2R-16 REPAIR 16 AND DWG 141A5502.;[02] VERIFIED COMPLETE
- [SDR SWAA2024071198007](https://openairdocs.org/sdr/SWAA2024071198007.md): Cargo Track · cracked · Jun 3, 2024 · N7737E · Boeing 7377BD · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO BAY CARGO TRACK IS CRACKED BS747 AND BS767 RBL13 WL155<[01] REMOVED AND REPLACED TRACK AS PER 737-700 SRM 53-00-53-3; EA 24-153-01519 AND DRAWING 146A7500 REV A.;[02] VERIFIED COMPLETION CORRECTIVE ACTION 1 AND MEASUREMENT TABLE.
- [SDR SWAA2024071198012](https://openairdocs.org/sdr/SWAA2024071198012.md): Strap · corroded · Jun 3, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY FLOOR SPLICE STRAP AROUND NUT PLATE HOLE BS727D+6 RBL11.5 WL156<[01] EVALUATED CORROSION ON FLOOR SPLICE STRAP BS 727D+6 RBL 11.5 WL 156; FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS IN THE SRM AND REQUIRES REPLACEMENT PER SRM 51-10-02-0G
- [SDR SWAA2024071198008](https://openairdocs.org/sdr/SWAA2024071198008.md): Support Plate · corroded · Jun 3, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156<[01] EVALUATED CORROSION; FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2; LOCATED DRILLED; APPLIED CHEMICAL CONVERSION COATING;
- [SDR SWAA2024071198000](https://openairdocs.org/sdr/SWAA2024071198000.md): Angle · cracked · Jun 3, 2024 · N7737E · Boeing 7377BD · Wing Miscellaneous Structure
  > RIGHT WING; I/B UPPER T/E PANEL JUST AFT OF REAR SPAR; UPPER U SUPPORT CHANEL FWD ATTACH ANGLE IS CRACKED<[01] 01 - REMOVED AND REPLACED PER [SRM 51-40-02-0G-0-A00729 (GENERAL - FASTENER INSTALLATION AND REMOVAL - AIRFRAME - PERMANENT)] RIGHT WING; I/B; UPPER
- [SDR SWAA2024071097642](https://openairdocs.org/sdr/SWAA2024071097642.md): Scuff Plate · cracked · Jun 2, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > FSD; SCUFF PLATE AFT SIDE IS CRACKED 3 INCHES.<[01] FUSION WELDED THE DAMAGED AREA ON SCUFF PLATE IAW SRM53-10-15-2R-2. PT INSPECTED WELDED AREA PER SOPM 20-20-02. NO CRACKS NOTED. SANDED THE REWORKED SURFACES AND EDGES OF SCUFF PLATE AS NECESSARY TO GET A SUR
- [SDR SWAA2024071197337](https://openairdocs.org/sdr/SWAA2024071197337.md): Floorboard · delaminated · Jun 1, 2024 · N7737E · Boeing 7377BD · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR BOARD 241ZF IS DELAMINATED<[01] PASSENGER CABIN FLOOR BOARD 241ZF WITH UPPER SKIN DELAMINATION WAS REPAIRED PER SRM 53-00-50-2R-1.;[02] JOB COMPLETE.
- [SDR SWAA2024071197339](https://openairdocs.org/sdr/SWAA2024071197339.md): Floorboard · delaminated · Jun 1, 2024 · N7737E · Boeing 7377BD · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR BOARD 242VF IS DELAMINATED<[01] DELAMINATION ON PASSENGER CABIN FLOOR PANEL 242VF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] VERIFIED CORRECTIVE ACTION #1
- [SDR SWAA2024071197340](https://openairdocs.org/sdr/SWAA2024071197340.md): Floorboard · delaminated · Jun 1, 2024 · N7737E · Boeing 7377BD · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR BOARD 242SF IS DELAMINATED<[01] DELAMINATED UPPER SURFACE OF PASSENGER CABIN FLOOR PANEL 242SF WAS REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.
- [SDR SWAA2024071197343](https://openairdocs.org/sdr/SWAA2024071197343.md): Floorboard · delaminated · Jun 1, 2024 · N7737E · Boeing 7377BD · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR BOARD 242AF IS DELAMINATED<[01] PASSENGER CABIN FLOOR BOARD 242AF WITH DELAMINATED WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 AND BDWG: 144A5810 ID: 0189. DUE TO AMOUNT OF ALL DAMAGE;[02] VERIFIED CORRECTIVE AC
- [SDR SWAA2024071197346](https://openairdocs.org/sdr/SWAA2024071197346.md): Floorboard · delaminated · Jun 1, 2024 · N7737E · Boeing 7377BD · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FLOOR BOARD 232RF IS DELAMINATED<[01] PASSENGER CABIN FLOOR BOARD 232RF WITH DELAMINATED WAS REPLACED WITH A NEWLY FABRICATED FLOOR PANEL PER SRM 53-00-50-2R-0 AND BDWG: 144A5810 ID: 0004 DUE TO AMOUNT OF ALL DAMAGE;[02] VERIFIED CORRECTIVE ACT
- [SDR SWAA2024071197336](https://openairdocs.org/sdr/SWAA2024071197336.md): Floorboard · delaminated · Jun 1, 2024 · N7737E · Boeing 7377BD · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR BOARD 241XF IS DELAMINATED<[01] DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER CABIN FLOOR BOARD 241XF IAW SRM 51-10-02-0G-0 PARA 9 AND DWG D1040M003.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2024071197338](https://openairdocs.org/sdr/SWAA2024071197338.md): Floor Panel · delaminated · Jun 1, 2024 · N7737E · Boeing 7377BD · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR BOARD 241UF IS DELAMINATED<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241UF FLOOR PANEL FROM BMS4-23 TYPE 2 LOT#1553922-1; INSTALLED ALL INSERTS USING BMS5-107 LOT#AK3BA2380A-A; CURED UNDER HEAT LAMP MONITORED WITH THERMOMETER ATS220
- [SDR SWAA2024071097341](https://openairdocs.org/sdr/SWAA2024071097341.md): Floor Panel · delaminated · Jun 1, 2024 · N7737E · Boeing 7377BD · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR BOARD 241EF IS DELAMINATED<[01] FABRICATED 241EF FLOORBOARD IAW SRM 53-00-50-2R-0 ALONG WITH DWG: 144A5810 SHEET: 129;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2024071097342](https://openairdocs.org/sdr/SWAA2024071097342.md): Floorboard · delaminated · Jun 1, 2024 · N7737E · Boeing 7377BD · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR BOARD 242DF IS DELAMINATED<[01] FABRICATED 242DF FLOORBOARD IAW SRM 53-00-50-2R-0 ALONG WITH DWG: 144A5810 SHEET: 3.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2024071097344](https://openairdocs.org/sdr/SWAA2024071097344.md): Floorboard · delaminated · Jun 1, 2024 · N7737E · Boeing 7377BD · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR BOARD 241BF IS DELAMINATED<[01] DUE TO EXTENT OF THE DAMAGE FABRICATED NEW 241BF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.
- [SDR SWAA2024071097345](https://openairdocs.org/sdr/SWAA2024071097345.md): Floorboard · delaminated · Jun 1, 2024 · N7737E · Boeing 7377BD · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR BOARD 241AF IS DELAMINATED<[01] DUE TO EXTENT OF DAMAGE FABRICATED NEW 241AF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] JOB COMPLETE.
- [SDR SWAA2024071097333](https://openairdocs.org/sdr/SWAA2024071097333.md): Floorboard · delaminated · Jun 1, 2024 · N7737E · Boeing 7377BD · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR BOARD 222B IS DELAMINATED<[01] DELAMINATIONS ON PASSENGER CABIN FLOOR BOARD 222B WERE REPAIRED IAW SRM 53-00-50-2R-1.;[02] JOB COMPLETE.

Next page: https://openairdocs.org/aircraft/N7737E/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 = 'N7737E' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7737E/reports

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