# Service difficulty reports: N7738A

A list on [N7738A](https://openairdocs.org/aircraft/N7738A.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 · 255 reports

- [SDR SWAA2026060809478](https://openairdocs.org/sdr/SWAA2026060809478.md): Flap System · faulted · Jun 4, 2026 · N7738A · Boeing 7377BD · Trailing Edge Flap Control System
  > ON APPROACH TO PVR HAD T/E FLAP DISAGREEMENT WHEN FLAP LEVER WAS SET TO POSITION 5. RAN QRH CHECKLIST. CW FSEU BITE WITH NO CURRENT OR EXISTING FAULTS PER FIM 27-51 TASK 801. ACFT HAS NO 30 DAY HISTORY. ACCOMPLISHED T/E FLAPS OP'S TEST IAW AMM 27-51-00. ACFT
- [SDR SWAA2026052204558](https://openairdocs.org/sdr/SWAA2026052204558.md): Cover · missing · May 19, 2026 · N7738A · Boeing 7377BD · Emergency Lighting
  > EMERGENCY EXIT LIGHT COVER LOWER LEFT SIDE MISSING. INSTALLED EMERGENCY EXIT LIGHT COVER ON LOWER LEFT SIDE OF RH EMERGENCY EXIT DOOR PER AMM 33-51-01.
- [SDR SWAA2026051898217](https://openairdocs.org/sdr/SWAA2026051898217.md): Battery · corroded · May 13, 2026 · N7738A · Boeing 7377BD · Emergency Equipment
  > FWD MEGA PHONE BATTERIES ARE CORRODED.<[01] REPLACED FWD MEGA PHONE BATTERIES I.A.W AMM 25-64-00. OPS CHECKS GOOD.
- [SDR SWAA2026050493463](https://openairdocs.org/sdr/SWAA2026050493463.md): Slide · out of adjust · Apr 28, 2026 · N7738A · Boeing 7377BD · Escape Slide
  > R 1 DOOR SLIDE Z FOLD FOR COVER IS INCORRECT NEEDS ADJUSTMENT. VERIFIED ADJUSTMENT OF Z FOLD IN TO R1 CORRECT POSITION IAW AMM 25-66-00;[02] ADJUSTED R1 DOOR SLIDE Z FOLD COVER IAW AMM 25-66-01.
- [SDR SWAA2026040786286](https://openairdocs.org/sdr/SWAA2026040786286.md): Lamp · inoperative · Apr 4, 2026 · N7738A · Boeing 7377BD · Emergency Lighting
  > EMERGENCY EXIT LIGHT AT ROW 15 FED INOPERATIVE. REPLACED THE LAMP AT THE OVERWING EXIT LIGHT ROW 15DEF IAW AMM 33-21-00, OPS CHECKED GOOD.
- [SDR SWAA2026040786285](https://openairdocs.org/sdr/SWAA2026040786285.md): Lamp · inoperative · Apr 4, 2026 · N7738A · Boeing 7377BD · Emergency Lighting
  > EMERGENCY EXIT LIGHT AT ROW 14 CB INOPERATIVE. REPLACED THE LAMP AT THE OVERWING EXIT LIGHT ROW 14ABC IAW AMM 33-21-00. OPS CHECKED GOOD.
- [SDR SWAA2026040285015](https://openairdocs.org/sdr/SWAA2026040285015.md): Slide · low pressure · Mar 30, 2026 · N7738A · Boeing 7377BD · Escape Slide
  > FWD SERVICE ESCAPE SLIDE PRESSURE IN RED. REPLACED FWD SERVICE DOOR EMERGENCY SLIDE ASSEMBLY WITH A SERVICEABLE UNIT IAW AMM 25-66-01 AND MT 725-61-06 AS REQUIRED.
- [SDR SWAA2026032380289](https://openairdocs.org/sdr/SWAA2026032380289.md): Lens · detached · Mar 17, 2026 · N7738A · Boeing 7377BD · Emergency Lighting
  > EMERGENCY EXIT LIGHTING LENS COVER AT ROW 23ABC CAME OFF. OK TO CONTINUE PER MEL 25-10-01. LIGHT STILL FULLY FUNCTIONAL. INSTALLED ROW 23ABC EMERGENCY AREA LIGHT LENS IAW AMM 33-51-03. OPS CHECK GOOD.
- [SDR SWAA2026030275216](https://openairdocs.org/sdr/SWAA2026030275216.md): Lens · missing · Feb 27, 2026 · N7738A · Boeing 7377BD · Emergency Lighting
  > 23 ABC EMERGENCY LIGHT COVER MISSING. EMERG LIGHT LENS AT 22ABC - 23ABC IS ON MEL.
- [SDR SWAA2026022674338](https://openairdocs.org/sdr/SWAA2026022674338.md): Lens · missing · Feb 25, 2026 · N7738A · Boeing 7377BD · Emergency Lighting
  > EMERGENCY LIGHT LENS ON OVERHEAD BIN BETWEEN 22ABC & 23ABC MISSING. OK TO CONT PER MEL 25-10-01 SP1B. REPLACED LENS IAW AMM 33-51-03. OP CHECK GOOD. THIS CLEARS MEL.
- [SDR SWAA2025121246012](https://openairdocs.org/sdr/SWAA2025121246012.md): Light · loose · Dec 9, 2025 · N7738A · Boeing 7377BD · Emergency Lighting
  > PASSENGER CABIN SEAT ROW 1 DEF PHOTOILLUM STRIP LOOSE AT RT FWD WINDSCREEN. SECURED THE STRIP IAW AMM 33-51-03.
- [SDR SWAA2025121243990](https://openairdocs.org/sdr/SWAA2025121243990.md): Light · loose · Dec 9, 2025 · N7738A · Boeing 7377BD · Emergency Lighting
  > PASSENGER CABIN SEAT ROW 1 DEF PHOTOILLUM STRIP LOOSE AT RIGHT FWD WIND SCREEN. SECURED LOOSE CABIN PHOTOILLUM STRIP IAW AMM 33-51-03.
- [SDR SWAA2025092416768](https://openairdocs.org/sdr/SWAA2025092416768.md): Light · inoperative · Sep 21, 2025 · N7738A · Boeing 7377BD · Emergency Lighting
  > ROW 1DEF PHOTOLUMINESCENT STRIP INOPERATIVE. REMOVED AND REPLACED IAW AMM 33-51-15-201-NG.
- [SDR SWAA2025030400451](https://openairdocs.org/sdr/SWAA2025030400451.md): Fitting · cracked · Feb 28, 2025 · N7738A · Boeing 7377BD · Main Landing Gear
  > LEFT CENTER GEAR DOOR CRACKED AT FWD FITTING <[01]. REMOVED L/H CTR/INNER GEAR DOOR ASSY. I.A.W. AMM 32-13-11 OK TO CONTINUE SERVICE PER CDL 32-10-3 XC.
- [SDR SWAA2024102953903](https://openairdocs.org/sdr/SWAA2024102953903.md): Cover · loose · Oct 26, 2024 · N7738A · Boeing 7377BD · Emergency Lighting
  > EMERGENCY EXIT LIGHT COVER LEFT SIDE OFF<[01] RESECURED CAPT SIDE EMER EXIT LIGHT COVER PER SIP.
- [SDR SWAA2024101647568](https://openairdocs.org/sdr/SWAA2024101647568.md): Cover · out of adjust · Oct 12, 2024 · N7738A · Boeing 7377BD · Escape Slide
  > PAX CABIN LEFT AFT SERVICE DOOR SLIDE COVER RUBBING AGAINST TO DOOR SCUFF PLATE TO CLOSE POSITION. 2024-565673<[01] INSTALLED CORRECTLY DOOR SLIDE COVER GIRT I.A.W B737-700 AMM 25-66-01-200-802; STEP 3.B.(1).(D).;[02] CERTIFIED WORK PERFORMED.
- [SDR SWAA2024101647567](https://openairdocs.org/sdr/SWAA2024101647567.md): Handle · loose · Oct 12, 2024 · N7738A · Boeing 7377BD · Service Doors
  > PAX CABIN AFT RIGHT SERVICE DOOR LINING;ASSISTANT HANDLE LOOSE. 2024-565671<[01] INSTALLED CORRECTLY ASSISTANT HANDLE PAX CABIN AFT RIGHT SERVICE DOOR LINING IAW B737-700 AMM 25-21-25-420-801 STEP 3(B) ITEM (5);[02] INSTALLED CORRECTLY ASSISTANT HANDLE PAX CA
- [SDR SWAA2024101647581](https://openairdocs.org/sdr/SWAA2024101647581.md): Light · inoperative · Oct 12, 2024 · N7738A · Boeing 7377BD · Emergency Lighting
  > EXTERIOR FUSELAGE FWD AREA RIGHT EMERGENCY LIGHT INOP 2024-565696<[01] REPLACED EXTERIOR FUSELAGE FWD AREA RIGHT EMERGENCY LIGHT IAW B737-700 AMM 33-51-04-960-802 AND PERFORMED TEST IS OK.SEE INDIVIDUAL SIGN OFF BELOW.;[02] CORRECTED STEP 1.<BR>REPLACED EXTER
- [SDR SWAA2024101647570](https://openairdocs.org/sdr/SWAA2024101647570.md): Handle · loose · Oct 12, 2024 · N7738A · Boeing 7377BD · Passenger/Crew Doors
  > PAX CABIN AFT ENTRY AREA AFT LEFT BULKHEAD O/B SIDE OF FA SEAT;ASSISTANT HANDLE LOOSE 2024-565682<[01] INSTALLED CORRECTLY ASSIT HANDLE ON PAX CABIN AFT ENTRY AREA AFT LEFT BULKHEAD O/B SIDE OF FA SEAT I.A.W. YOKOHAMA CMM 25-42-76 REV 05 ASSEMBLY STEP 1.M. PA
- [SDR SWAA2024101644930](https://openairdocs.org/sdr/SWAA2024101644930.md): Seat · out of adjust · Oct 4, 2024 · N7738A · Boeing 7377BD · Passenger Compartment Equipment
  > RECLINE SEAT 11C EMERGENCY EXIT PASSENGER SEAT 2024-565614<[01] PERFORMED ADJUSTMENT ON PASSENGER SEAT 11C EMERGENCY EXIT PASSENGER SEAT IAW CMM 25-21-45 B/E AEROSPACE REV. 5 ITEM 3. G. (3) PAGE 6005.;[02] TASK CARD COMPLETED <BR>PERFORMED ADJUSTMENT ON PASSEN
- [SDR SWAA2024101644929](https://openairdocs.org/sdr/SWAA2024101644929.md): Rib · cracked · Oct 3, 2024 · N7738A · Boeing 7377BD · Horizontal Stabilizer, Spar/Rib
  > CRACK ON INSPAR RIB 129.50 MORE 34 INCH FROM TO FRONT SPAR RT HORIZONTAL STABILIZER 2024-565613<[01] TOOL USED ON STEP 3 AND 4:EDDY CURRENT FLAW DETECTOR P/N:NORTEC 600D; S/N:210138103;DUE DATE:10-JUN-25.;[02] PERFORMED PERMANENT REPAIR ON INSPAR RIB 129.50 MO
- [SDR SWAA2024101642350](https://openairdocs.org/sdr/SWAA2024101642350.md): Floor Support · cracked · Sep 27, 2024 · N7738A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK ON HOLE OF INTERCOSTAL LOCATED BS 251.6 AND LBL 16 FLIGHT DECK FLOOR 2023-565606<[01] REPLACED INTERCOSTAL LOCATED BTW BS 251.6 AND LBL 15.3 AT LBL 24.7 FLIGHT DECK FLOOR IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 141A5100; SHEET132; REV A. SEE INDIVIDUAL
- [SDR SWAA2024101641390](https://openairdocs.org/sdr/SWAA2024101641390.md): Web · cracked · Sep 24, 2024 · N7738A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK FLOOR STRUCTURE WEB STA 291.5 TO STA 332.10 AT LEVEL OF STR17R AT FWD GALLEY AREA 2024-565603<[01] REPLACED WEB STA 291.5 TO STA 332.10 AT LEVEL OF STR17R AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DRAWING 141A8310 REV:B.SEE INDIVIDUAL STEP SIGN O
- [SDR SWAA2024101639384](https://openairdocs.org/sdr/SWAA2024101639384.md): Vapor Barrier · cracked · Sep 20, 2024 · N7738A · Boeing 7377BD · Fuselage Main, Bulkhead
  > CRACK INDICATION FOUND ON VAPOR BARRIER LOWER WEB AT BS 663 AND LBL 50 CRACK LENGTH IS 5 INCH 2024-565593<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: A24028535; DUE DATE: 06-JUN-25.;[02] TOOL USED= HOT BONDER P/N: HCS9200B; S/N: 16122983; DUE DATE: 15-FEB-25
- [SDR SWAA2024101637137](https://openairdocs.org/sdr/SWAA2024101637137.md): Floor Support · corroded · Sep 12, 2024 · N7738A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > AAI-INSPECTION AFT CARGO COMPARTMENT; FLOOR SUPPORT BRACKET HAS CORROSION BWT STA 847 & STA 867; STR 25R 2024-565563<[01] REPLACED SUPPORT BRACKET AND FASTENER LOCATED BTW STA847 AND STA867 STR25R IAW B737-700 SRM 51-10-02 ITEM 9 AND DRAWING 146A8320 REV-: SEE
- [SDR SWAA2024101637138](https://openairdocs.org/sdr/SWAA2024101637138.md): Floorbeam · cracked · Sep 12, 2024 · N7738A · Boeing 7377BD · Fuselage Main, Floor Beam
  > AAI-INSPECTION PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75 2024-565565<[01] REPLACED BRAKE CHANNEL LOCATED ON BS 540; BL 0 TO RBL 24.75 AND FASTENERS IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. SEE INDIVIDUAL SIGN OF
- [SDR SWAA2024101637139](https://openairdocs.org/sdr/SWAA2024101637139.md): Floor Support · cracked · Sep 12, 2024 · N7738A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > AAI-INSPECTION PASSENGER CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75 2024-565566<[01] REPLACED BRAKE CHANNEL LOCATED ON BS 540; BL 0 TO LBL 24.75 IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 Ï¿½TEM 9. SEE INDIVIDUAL SIGN OFF BELOW;[02]
- [SDR SWAA2024101637131](https://openairdocs.org/sdr/SWAA2024101637131.md): Access Panel · cracked · Sep 12, 2024 · N7738A · Boeing 7377BD · Horizontal Stabilizer, Plate/Skin
  > CRACK BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB 2024-565546<[01] REPLACED BLADE ACCESS PANEL 343AT AT RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02;[02] TASK COMPLETED.
- [SDR SWAA2024101636640](https://openairdocs.org/sdr/SWAA2024101636640.md): Access Panel · cracked · Sep 11, 2024 · N7738A · Boeing 7377BD · Wing, Plate/Skin
  > CRACK ANGLE TRAILING EDGE ACCESS PANEL 651GB RT WING 2024-565519<[01] REPLACED ANGLE TRAILING EDGE ACCESS PANEL 651GB ON RT WING I.A.W B737-700 SRM 51-40-02 AND DWG 115A2714-16 REV. -;[02] CORRECTED STEP 1:<BR>REPLACED ANGLE TRAILING EDGE ACCESS PANEL 651GB ON
- [SDR SWAA2024101636053](https://openairdocs.org/sdr/SWAA2024101636053.md): Angle · cracked · Sep 10, 2024 · N7738A · Boeing 7377BD · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED ORSS 273 LT WING 2024-565491<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 273 LT WING IAW B737-700 SRM 51-40-02 AND B737-700 SRM 51-10-02 ITEM 9; AND MESURE OF CRACK IS: L: 0.221 INCH TOOK MECHANICALLY TOOL USED CALIPER P/N:
- [SDR SWAA2024101035684](https://openairdocs.org/sdr/SWAA2024101035684.md): Placard · deteriorated · Sep 9, 2024 · N7738A · Boeing 7377BD · Placards and Markings
  > DETERIORATED PLACARD CAUTION ESCAPE SLIDE ON SLIDE COVER FWD ENTRY DOOR (1EA) 2024-565485<
- [SDR SWAA2024101635238](https://openairdocs.org/sdr/SWAA2024101635238.md): Bracket · cracked · Sep 7, 2024 · N7738A · Boeing 7377BD · Leading Edge Devices
  > CRACK SLAT 2 O/B AUXILIARY TRACK I/B SUPPORT ANGLE AT LT WING 2024-565422<[01] REPLACED BRACKET LOC. SLAT 2 O/B AUXILIARY TRACK I/B SUPPORT ANGLE AT LT WING I.A.W. B737-700 CMM 57-43-02 STEP 2.C ITEM 9 FIGURE 701 SHEET 2 OF 2 PAG 710. THR MEASURE OF CRACK IS:1
- [SDR SWAA2024101634950](https://openairdocs.org/sdr/SWAA2024101634950.md): Support Angle · cracked · Sep 6, 2024 · N7738A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT BS 727B AND LBL 52 CEILING AREA AFT CARGO COMPARTMENT 2024-565342<[01] STEP 6 TOOL USED EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 210138503; CAL DUE DATE: 05-AUG-25;[02] PERFORMED REPAIR ON ANGLE-SUPPORT LOCATED BTW BS 727A TO BS 747
- [SDR SWAA2024101634955](https://openairdocs.org/sdr/SWAA2024101634955.md): Cargo Track · cracked · Sep 6, 2024 · N7738A · Boeing 7377BD · Fuselage, Seat/Cargo Attach Fittings
  > CRACK TRACK RBBL 13.84 AND BS 747 AFT CARGO COMPARTMENT 2024-565348<[01] FAULT RESOLVED IN OTHER FAULT SEE TTG8Q00VPXBM;[02] CORRECTED ITEM 1: FAULT RESOLVED IN OTHER FAULT DUE TO THIS DAMAGE (CRACK) IS ON BS767 AND THE CARGO TRACK SECTION AND WILL BE REPAIRED
- [SDR SWAA2024101634948](https://openairdocs.org/sdr/SWAA2024101634948.md): Handle · broken · Sep 6, 2024 · N7738A · Boeing 7377BD · Service Doors
  > BROKEN DOOR LINING HANDLE AFT SERVICE DOOR AT AFT GALLEY AREA (1 EA) 2024-565228<[01] REPLACED DOOR LINING HANDLE AFT SERVICE DOOR AT AFT GALLEY AREA (1 EA) I.A.W B737-700 AMM 25-21-25-420-801; STEP 3.B.(5).;[02] REPLACED DOOR LINING HANDLE AFT SERVICE DOOR AT
- [SDR SWAA2024101634954](https://openairdocs.org/sdr/SWAA2024101634954.md): Cargo Track · cracked · Sep 6, 2024 · N7738A · Boeing 7377BD · Fuselage, Seat/Cargo Attach Fittings
  > CRACK TRACK RBBL 13.84 AND BS 727E AFT CARGO COMPARTMENT 2024-565347<[01] TOOL USED ON STEP 4: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600D; S/N: 60009161631; DUE DATE: 11-MAR-25;[02] REPAIRED CARGO TRACK RBBL13.84 FROM STA 727D+5 INCHES TO STA 767+ 17 INCHES
- [SDR SWAA2024101634951](https://openairdocs.org/sdr/SWAA2024101634951.md): Floorbeam · corroded · Sep 6, 2024 · N7738A · Boeing 7377BD · Fuselage Main, Floor Beam
  > CORROSION FLOOR BEAM LOCATED STA986.5 AND LBL43 WL208.1 AT AFT GALLEY AREA 2024-565332<[01] TOOL USED: EDDY CURRENT FLAW DETECTOR; P/N: NORTEC 600 D; S/N: 200048001; DUE DATE: 28-MAY-25.;[02] ON STEP 10. TOOL USED: ET INSTRUMENT. P/N: NORTEC 600D. S/N: 2202725
- [SDR SWAA2024101634952](https://openairdocs.org/sdr/SWAA2024101634952.md): Floorbeam · corroded · Sep 6, 2024 · N7738A · Boeing 7377BD · Fuselage Main, Floor Beam
  > CORROSION FLOOR BEAM LOCATED STA986.5 AND RBL33 TO RBL43 WL208.1 AT AFT GALLEY AREA 2024-565333<[01] TOOL USED IN STEP 5; TOOL USED: ULTRASONIC THICKNESS GAGES; P/N:45MG; S/N:232017609; CAL DUE DATE: 22-SEP-24;[02] ON STEP 9 AND 10. TOOL USED: ET INSTRUMENT. P
- [SDR SWAA2024101634956](https://openairdocs.org/sdr/SWAA2024101634956.md): Cargo Track · cracked · Sep 6, 2024 · N7738A · Boeing 7377BD · Fuselage, Seat/Cargo Attach Fittings
  > CRACK TRACK RBBL 13.84 AND BS 767 AFT CARGO COMPARTMENT 2024-565349<[01] FAULT RESOLVED IN OTHER FAULT SEE TTG8Q00VPXBM;[02] CORRECTED ITEM 1: FAULT RESOLVED IN OTHER FAULT DUE TO THIS DAMAGE (CRACK) IS ON BS767 AND THE CARGO TRACK SECTION AND WILL BE REPAIRED
- [SDR SWAA2024101634958](https://openairdocs.org/sdr/SWAA2024101634958.md): Bracket · cracked · Sep 6, 2024 · N7738A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK FLOOR STRUCTURE BRACKET BS 947.5 AND STRINGER 25L AT AFT CARGO COMPARTMENT 2024-565352<[01] REPLACED FLOOR STRUCTURE BRACKET AND FASTENERS LOCATED BTW BS 947.5 AND STRINGER 25L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND DWG 149A8103; SHEET 7;
- [SDR SWAA2024101634957](https://openairdocs.org/sdr/SWAA2024101634957.md): Support Angle · cracked · Sep 6, 2024 · N7738A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT BETWEEN BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AFT CARGO COMPARTMENT 2024-565351<[01] REPLACED ANGLE-SUPPORT (STIFFENER) AND FASTENERS LOCATED BTW BS 907 TO BS 927 STRINGER 25R AND STRINGER 27R AFT CARGO COMPARTMENT IAW B737-700 S
- [SDR SWAA2024101634869](https://openairdocs.org/sdr/SWAA2024101634869.md): Angle · cracked · Sep 6, 2024 · N7738A · Boeing 7377BD · Aerodynamic Fairings
  > CRACK SUPPORT STRUCTURE WING TO BODY FAIRING ANGLE BS 500D AT LEVEL STRINGER 19R AT LOWER FUSELAGE 2024-565327<[01] REPLACED SUPPORT STRUCTURE WING TO BODY FAIRING ANGLE BS 500D AT LEVEL STRINGER 19R AT LOWER FUSELAGE I.A.W. B737-700 SRM 51-40-02 AND DRAWING #
- [SDR SWAA2024101634870](https://openairdocs.org/sdr/SWAA2024101634870.md): Angle · cracked · Sep 6, 2024 · N7738A · Boeing 7377BD · Aerodynamic Fairings
  > CRACK SUPPORT STRUCTURE WING TO BODY FAIRING ANGLE BS 500D AT LEVEL STRINGER 19L AT LOWER FUSELAGE 2024-565328<[01] REPLACED SUPPORT STRUCTURE WING TO BODY FAIRING ANGLE BS 500D AT LEVEL STRINGER 19L AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02-0G-0 AND DRAWING
- [SDR SWAA2024101634640](https://openairdocs.org/sdr/SWAA2024101634640.md): Stub Frame · cracked · Sep 5, 2024 · N7738A · Boeing 7377BD · Fuselage Main, Frame
  > CRACK STUB FRAME LOCATED STA294.5 AND STR17R AT PASSENGER CABIN 2024-565307<[01] EQUIPMENT P/N PHASEC 3D; S/N 587435/07; DUE DATE 20-MAR-25 WAS USED ON STEP 7;[02] TOOL USED: EDDY CURRENT EQUIPMENT; P/N: NORTEC600D; S/N: 220272512; CAL DUE DATE: 08-JAN-25;[03]
- [SDR SWAA2024101634644](https://openairdocs.org/sdr/SWAA2024101634644.md): Stub Frame · cracked · Sep 5, 2024 · N7738A · Boeing 7377BD · Fuselage Main, Frame
  > CRACK INDICATIONS ON STUB FRAME LOCATED ON BS 294.5 BTW S-8R T O S-9R (2 EA) AT FWD GALLEY DOOR AREA CRACKS LENGTH 0.312 IN.AT PASSENGER CABIN 2024-565314<[01] REPLACED STUB FRAME LOCATED ON BS 294.5 BTW S-7R TO S-9R AT FWD GALLEY SERVICE DOOR AREA IAW B737-70
- [SDR SWAA2024101634457](https://openairdocs.org/sdr/SWAA2024101634457.md): Support Angle · cracked · Sep 5, 2024 · N7738A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED STA695 AND LBL24.75 CENTER SECTION 2024-565246<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 14282005 DUE DATE 22 JAN 25; P/N P3015GOES00000 S/N 142031023 DUE DATE 22 JAN 25.;[02] REPLACED SUPPORT ANGLE AND FASTENERS
- [SDR SWAA2024101634637](https://openairdocs.org/sdr/SWAA2024101634637.md): Intercostal · cracked · Sep 5, 2024 · N7738A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK WEB INTERCOSTAL LOCATED BETWEEN STA294.5 TO STA303.9 AND STR16L AT PASSENGER CABIN 2024-565293<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 142811020 DUE DATE 23 JAN 25; P/N P3015GOES00000 S/N 112820025 DUE DATE 22 JAN 25.;[02] REPLACED
- [SDR SWAA2024101634455](https://openairdocs.org/sdr/SWAA2024101634455.md): Floor Support · cracked · Sep 5, 2024 · N7738A · Boeing 7377BD · Fuselage Miscellaneous Structure
  > CRACK ANGLE FLOOR STRUCTURE LOCATED STA695 AND BL0 WL208.1 CENTER SECTION 2024-565243<[01] TOOL USED: TEMPERATURE CONTROLLER P/N P3015GOES00000 S/N 14282005 DUE DATE 22 JAN 25; P/N P3015GOES00000 S/N 142031023 DUE DATE 22 JAN 25.;[02] REPLACED NEW ANGLE FLOOR
- [SDR SWAA2024101634645](https://openairdocs.org/sdr/SWAA2024101634645.md): Bear Strap · cracked · Sep 5, 2024 · N7738A · Boeing 7377BD · Fuselage Main, Plate/Skin
  > CRACK INDICATION ON BEAR STRAP FORWARD GALLEY DOOR AREA BS 290-296 BETWEEN S-8R AND S-9R AT PASSENGER CABIN.CRACK LENGTH 0.375 IN.(1EA) 2024-565315<[01] STEP 5 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 210138503; DUE DATE:05-AUG-25;[02] TOOL USED E
- [SDR SWAA2024101634454](https://openairdocs.org/sdr/SWAA2024101634454.md): Rib · cracked · Sep 5, 2024 · N7738A · Boeing 7377BD · Horizontal Stabilizer, Spar/Rib
  > CRACK INSPAR RIB 111.10 LOCATED AT 28 INCHES OF FRONT SPAR AT RT HORIZONTAL STABILIZER 2024-565244<[01] TOOL USED ON STEP 3 AND 4 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 220272512; CAL DUE DATE: 08-JAN-25;[02] TOOL USED ON STEP 6 ET EQUIPMENT: P/N: NORTEC 600D; S

Next page: https://openairdocs.org/aircraft/N7738A/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 = 'N7738A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N7738A/reports

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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.