# Service difficulty reports: N918UP, cancelled Nov 21, 2007

A list on [N918UP, cancelled Nov 21, 2007](https://openairdocs.org/deregistered/N918UP-2007-11-21.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 3 · 135 reports

- [SDR UPS06247834](https://openairdocs.org/sdr/UPS06247834.md): Light · no test · Aug 29, 2006 · N918UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED C/P PORTABLE EMERGENCY LIGHT ASSY IAW MM 33-50-67-2. SYS OPS CKS OK.
- [SDR UPS06247826](https://openairdocs.org/sdr/UPS06247826.md): Lamp · failed · Aug 28, 2006 · N918UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:NA EMERGENCY LIGHT ABOVE CREW ENTRY DOOR DIM, RELAMPED. OPS CK NORMAL IAW 25 60 00.
- [SDR UPS06246793](https://openairdocs.org/sdr/UPS06246793.md): Light · inoperative · May 4, 2006 · N918UP · Boeing 72730C · Emergency Lighting
  > EMERGENCY EXIT LIGHT CAME OUT OF SOCKET. REINSTALLED ASSEMBLY. OPS CK GOOD PER AMM 33-50-01-5.
- [SDR 2006FA0000645](https://openairdocs.org/sdr/2006FA0000645.md): Control Valve · failed · Nov 8, 2005 · N918UP · Boeing 72730C · Extinguishing System
  > NR 2 ENGINE FIRE EXTINGUISHING SELECTOR CONTROL VALVE FAILED TO OPEN DURING ROUTINE TESTING IAW UPS ROUTINE TASK CARD TC 2-221-12. THE VALVE SOLENOID HOUSING WAS NOTED AS BEING CORRODED. (K)
- [SDR UPS05245823](https://openairdocs.org/sdr/UPS05245823.md): Stringer · corroded · Nov 1, 2005 · N918UP · Boeing 72730C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C STRINGER 24 RT FOUND CORRODED AT BS 725. PLEASE INVESTIGATE DAMAGE FOUND TO BE BEYOND LIMITS IAW SRM 53-10-3. DAMAGED SECTION OF STRINGER 24R CUT OUT AND REMOVED. AREA REPAIRED IAW 53-10-3 FIG 1 DETAIL 1 PAGE 4B.
- [SDR UPS05245859](https://openairdocs.org/sdr/UPS05245859.md): Skin · cracked · Oct 25, 2005 · N918UP · Boeing 72730C · Cargo/Baggage Doors
  > INSPECTION TYPE:C AFT CARGO DOOR CRACK ON INNER SKIN SECOND INSPECTION HOLE FWD EDGE AT BOTTOM. REMOVE FASTENER AND CHECK DEPTH OF CRACK TO DETERMINE REPAIR. HFEC CARRIED OUT AND CRACK FOUND CONTAINED WITHIN FASTENER HOLE. REPAIRED IAW SRM 51-40-02.
- [SDR UPS05245826](https://openairdocs.org/sdr/UPS05245826.md): Intercostal · cracked · Oct 24, 2005 · N918UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C STA 660, ST 29R REPAIR TO INTERCOSTAL IS CRACKED. PLEASE REPAIR IAW SRM. REPAIR BRACKET FABRICATED IAW SRM 51-20-071 FIG 7. REPAIR BRACKET REPLACED IAW SRM 51-30-02.
- [SDR UPS05245861](https://openairdocs.org/sdr/UPS05245861.md): Link · cracked · Oct 18, 2005 · N918UP · Boeing 72730C · Main Landing Gear
  > INSPECTION TYPE:C RT MLG UPLOCK FWD SUPPORT LINKS CRACKED. REPLACE LINKS. RT MLG UPLOCK FWD SUPPORT LINKS REPLACED IAW MM 20-80-01.
- [SDR UPS05245851](https://openairdocs.org/sdr/UPS05245851.md): Spar · corroded · Oct 16, 2005 · N918UP · Boeing 72730C · Wing Spar
  > AREA OF SUSPECT CORROSION ON WING CENTER SECTION REAR SPAR LWR CHORD BS 870 RBL36 DUE TO 2 POPPED FASTENER HEADS. PLEASE INVESTIGATE AND RECTIFY AS NECESSARY. AS PER BOEING INSTRUCTIONS THE LWR CHORD WAS REPLACED. NEW CHORD WAS CUT AT RBL 9.5. REPAIR SPLICE
- [SDR UPS05245832](https://openairdocs.org/sdr/UPS05245832.md): Skin · corroded · Oct 16, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > EVIDENCE OF CORROSION AT BS 360 STR 22L AT FWD END OF STR AT AFT FACE OF FRAME. PLEASE INVESTIGATE AND RECTIFY. CORROSION BLENDED OUT IAW SRM 51-10-06. CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-1. REPAIR STRAP FABRICATED IAW SRM 51-20-1 FIG 7. M
- [SDR UPS05245821](https://openairdocs.org/sdr/UPS05245821.md): Skin · corroded · Oct 16, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C NDT INSPECTION HAS INDICATION OF MATERIAL LOSS AT BS 441 FWD OF CENTER LINE AT STR 8L, INVESTIGATE. CORROSION FOUND BETWEEN SKIN AND DOUBLER. CORROSION REMOVED AND FOUND BE WITHIN LIMITS, AREA REPROTECTED IAW SRM 51-30-02.
- [SDR UPS05245836](https://openairdocs.org/sdr/UPS05245836.md): Trunnion · cracked · Oct 15, 2005 · N918UP · Boeing 72730C · Fuselage, Landing Gear Attach Fittings
  > RT TRUNNION ATTACH FITTING HAS CRACK AT OB FLANGE HOLE E RUNNING UP APPROX 2.5 INCHES. REMOVE AND REPLACE FITTING. RT TRUNNION FITTING FOUND CRACKED OUTSIDE REPAIRABLE LIMITS IN UPS EO B727-5740-20666C. REPLACED IAW UPS AUTHORIZATION B727-5740-23046-B.
- [SDR UPS05245831](https://openairdocs.org/sdr/UPS05245831.md): Skin · corroded · Oct 14, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > SURFACE CORROSION ON LAP JOINT BETWEEN S-4L AND 5L AT LOCATIONS BETWEEN BS 852 AND 1011. CORROSION REMOVED IAW SRM 51-10-2 (.002") AND FOUND WITHIN LIMITS IAW SRM 51-20-4.
- [SDR UPS05245824](https://openairdocs.org/sdr/UPS05245824.md): Support · corroded · Oct 14, 2005 · N918UP · Boeing 72730C · Fuselage, Landing Gear Attach Fittings
  > INSPECTION TYPE:C RT MLG TRUNNION BUTTERFLY FITTING HAS CORROSION. PLS REPLACE. SUPPORT REPLACED IAW DRW 65-19296.
- [SDR UPS05245860](https://openairdocs.org/sdr/UPS05245860.md): Bushing · cracked · Oct 13, 2005 · N918UP · Boeing 72730C · Engine Mount Section
  > INSPECTION TYPE:C ENGINE NR 3 AFT MOUNT FITTING HAS CORROSION ON INNER SURFACE OF UPPER USHING. REPLACE BUSHING. REPLACED BUSHING IAW OHM 20-50-03.
- [SDR UPS05245827](https://openairdocs.org/sdr/UPS05245827.md): Mount · corroded · Oct 13, 2005 · N918UP · Boeing 72730C · Engine Mount Section
  > INSPECTION TYPE:C ENGINE NR 3 FWD MOUNT FITTING HAS PITTING CORROSION ON BOTH OUTBOARD HOLES. REPAIR. REPAIRED IAW EO B727-5540-11592-A.
- [SDR UPS05245833](https://openairdocs.org/sdr/UPS05245833.md): Skin · corroded · Oct 12, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > AREA OF SUSPECT CORROSION ON CROWN SKIN BS 521 TO BS 515 BETWEEN STR 2L AND 3L. PLEASE PAINT STRIP AREA, REMOVE FASTENERS IF REQUIRED, REINSPECT AND RECTIFY AS NECESSARY. REPAIRED IAW UPS AUTHORIZATION B727-5330-23323-A
- [SDR UPS05245822](https://openairdocs.org/sdr/UPS05245822.md): Support Fitting · cracked · Oct 12, 2005 · N918UP · Boeing 72730C · Wing, Attach Fittings
  > RT WING FRONT SPAR TO BODY FITTING HAS SUSPECT CRACK ON OUTBD SIDE OF BOTTLE PIN. FITTING REPLACED IAW DWG 65C13724 AND UPS EO B727-5310-7477.
- [SDR UPS05245835](https://openairdocs.org/sdr/UPS05245835.md): Trunnion · cracked · Oct 11, 2005 · N918UP · Boeing 72730C · Fuselage, Landing Gear Attach Fittings
  > LT MLG SUPPORT FITTING HAS CRACK INDICATION IN HOLE B & C ON INB FLANGE AND HOLES E IN COUNTERSINKS. REPAIR AND REPLACE FITTING LT MLG TRUNNION REMOVED AND FOUND CRACKED OUTSIDE REPAIRABLE LIMITS IN UPS EO B727-5740-20666C. TRUNNION REPAIRED IAW UPS AUTHORIZ
- [SDR UPS05245829](https://openairdocs.org/sdr/UPS05245829.md): Skin · cracked · Oct 11, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C NDT INDICATES 2 CRACKS EMINATING FROM FASTENERS " BS235.8 STR16L-17L. PLEASE REPAIR IAW SRM 53-30-3 FIG 3. FASTENERS REMOVED FROM AFFECTED AREA IAW SRM 51-80-02. AFFECTED AREA CUTOUT IAW SRM 53-30-3. HFEC CARRIED OUT AROUND CUTOUT AND ON
- [SDR UPS05245828](https://openairdocs.org/sdr/UPS05245828.md): Skin · cracked · Oct 11, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SUSPECT SKIN CRACKS AT UPPER FWD CORNER OF FWD ENTRY DOOR CUT OUT BETWEEN STR 7L AND 8L. PLEASE CARRY OUT NDI AND RECTIFY AS NECESSARY IAW SRM ADDENDUM. HFEC CARRIED OUT IAW NDTM 51-00-00 PT6 FIG 4. TWO CRACKS FOUND. DAMAGE REMOVED IAW EO
- [SDR UPS05245834](https://openairdocs.org/sdr/UPS05245834.md): Skin · cracked · Oct 9, 2005 · N918UP · Boeing 72730C · Service Doors
  > FOUND SKIN CRACK AT FASTENER HOLE IN MID GALLEY DOOR CUT OUT, UPPER FWD CORNER. PLEASE CONFIRM WITH NDI AND RECTIFY AS NECESSARY HFEC CARRIED OUT ON FASTENER HOLES COMMON TO REPAIR IAW 727NDTM 51-00- 00 PT6 FIG 16. THREE CRACKS FOUND. REPAIR CARRIED OUT IAW
- [SDR UPS04241790](https://openairdocs.org/sdr/UPS04241790.md): Light · inoperative · Jan 29, 2004 · N918UP · Boeing 72730C · Emergency Lighting
  > BOTH EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REPLACED BATTERIES, OPS CHECK'S NORMAL.
- [SDR UPS03241453](https://openairdocs.org/sdr/UPS03241453.md): Warning Light · illuminated · Oct 21, 2003 · N918UP · Boeing 72730C · Smoke Detection
  > INSPECTION TYPE:N/A LOWER CARGO MX LIGHT ILLUMINATED INFLIGHT, MAINT. CODES DISPLAYED; A3398. SYSTEM TEST NORMAL PER MM 26-18-00. TESTED SEVERAL TIMES DURING LAYOVER PERIOD WITH NO DEFECTS NOTED AT THIS TIME DI 268782 CLOSED
- [SDR UPS03241350](https://openairdocs.org/sdr/UPS03241350.md): Light · inoperative · Oct 6, 2003 · N918UP · Boeing 72730C · Emergency Lighting
  > EVACUATION SLIDE ILLUMINATION LIGHT IS INOPERATIVE. REF TO WDM 33-50-02, EVACUATION SLIDE ILLUMINATION LIGHT IS ONLY A PROVISION.
- [SDR UPS01236693](https://openairdocs.org/sdr/UPS01236693.md): Control Unit · malfunctioned · Aug 23, 2001 · N918UP · Boeing 72730C · Rudder Control System
  > WITH RUDDER TRIMMED TO ZERO 12 DEGREE LEFT AILERON REQUIRED TO HOLD WINGS LEVEL DEPLOYING SPEED BRAKE SLIGHTLY FIXES PROBLEM. INSPECTED SPOILERS NO DEFECTS FOUND INSPECTED FLIGHT CONTROLS GEN MX PRACTICES 27-00-00 PAGE 201, 203 NO DEFECT FOUND HOWEVER SUS
- [SDR UPS01236443](https://openairdocs.org/sdr/UPS01236443.md): Battery · discharged · Jul 28, 2001 · N918UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHTS EXTINGUISH SHORTLY AFTER TURNED ON. REPLACED BATT IN FWD AFT EMERG LIGHT ASSY OPS CHECKS GOOD.
- [SDR UPS01235624](https://openairdocs.org/sdr/UPS01235624.md): Stringer · corroded · Mar 29, 2001 · N918UP · Boeing 72730C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C, FWD CARGO COMPT BETWEEN STA 680 AND 660, LT SIDE STRINGER 24, CORROSION. CUT OUT SECTION AT BAD STRINGER AREA STA 680 TO STA 660 LT STRINGER 24 INSTALLED REPAIR AS PER B727 SRM 53-10-3 FIG 1 SIDE OF STRINGER DOUBLER REPAIR 11 1/4 INCHES
- [SDR UPS01235625](https://openairdocs.org/sdr/UPS01235625.md): Keelbeam · cracked · Mar 28, 2001 · N918UP · Boeing 72730C · Fuselage Main, Keel
  > INSPECTION TYPE:C, RT SIDE OF KEELBEAM APU CUT OUT FWD END HAS A DOUBLER CRACKED AT BS 874 NEXT TO HORIZONTAL STIFFENER. REMOVED OLD DOUBLER REPAIR OF KEEL BEAM AREA AND INSTALLED NEW DOUBLER REPAIR AT SAME AREA BS 874 AS PER B727 SRM 51-10-01.
- [SDR UPS01235623](https://openairdocs.org/sdr/UPS01235623.md): Web · cracked · Mar 27, 2001 · N918UP · Boeing 72730C · Wing, Center Box
  > INSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION APROX 770 AND LBL 13 WEB IS CORRODED. REMOVED WEB AT LOWER FUSELAGE CENTER SECTION AT BS 770 AND LBL13 WEB AS PER B727 SRM 51-30-02. REPLACED DAMAGE WEB LOWER CENTER WING AT BS 770 AND LBL 13 WEB AS PER B 7
- [SDR UPS01235622](https://openairdocs.org/sdr/UPS01235622.md): Web · cracked · Mar 27, 2001 · N918UP · Boeing 72730C · Wing, Center Box
  > INSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION APROX BETWEEN BS 800 TO 810 AND LBL 13 WEB IS CORRODED. REMOVE WEB AT LWR FUSELAGE CENTER SECTION BETWEEN BS 800 TO BS 810 LBL 13 WEB AS PER B727 SRM 51-30-2. REPLACED DAMAGED WEB LOWER CENTER WING AT BS
- [SDR UPS01235621](https://openairdocs.org/sdr/UPS01235621.md): Web · cracked · Mar 27, 2001 · N918UP · Boeing 72730C · Wing, Center Box
  > INSPECTION TYPE:C LOWER F.S. AT WING CENTER SECTION BETWEEN BS 775 TO BS 800 AND RBL 13 WEBS CRACKED AND CORRODED. REMOVE WEB AT LWR FUSELAGE CENTER SECTION BETWEEN 767 TO 830 RBL13 AS PER B727 SRM 51-30-02 REMEOVED AND REPLACED DAMAGE WEB LOWER CENTER WING
- [SDR UPS01235628](https://openairdocs.org/sdr/UPS01235628.md): Seat Track · gouged · Mar 26, 2001 · N918UP · Boeing 72730C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C, MAIN CARGO DECK FUSELAGE STATION 1130 LBL 45 SEAT TRACK TONGUES ARE NICKED AND GOUGED REPLACED DAMAGED SECTION OF SEAT TRACK FROM BS 1110 TO STA 1130 LBL 45
- [SDR UPS01235626](https://openairdocs.org/sdr/UPS01235626.md): Pressure Panel · cracked · Mar 26, 2001 · N918UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, NOSE WHEEL WELL RT SIDE CRACKED AT BS 286.5 TO BS 294.5 WL 160 LOOKING FROM INSIDE TUNNEL. CUT OUT DAMAGE AREA, NDT CUT OUT, AND INSTALLED DOUBLER REPAIR AS PER B727 SRM 51-40-2 FIG.1
- [SDR UPS00234210](https://openairdocs.org/sdr/UPS00234210.md): Pulley · worn · Oct 20, 2000 · N918UP · Boeing 72730C · Trailing Edge Flap Control System
  > INSPECTION TYPE:N/A, ATB DURING FLAP RETRACTION OUTBOARD FLAPS WENT TO 2 DEGREES, MATCHED FL AND LE, INBOARD FLAPS JAMMED AT R-5 DEGREES L-15 DEGREES. REMOVED AND REPLACED LEFT INBOARD FLAP TRANSMITTER CABLE AND PULLEY PER MM 27-52-02. OPS CK NORMAL.
- [SDR UPS00233553](https://openairdocs.org/sdr/UPS00233553.md): Light · inoperative · Aug 9, 2000 · N918UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSEMBLE AND BATTERIES OPS CK GOOD.
- [SDR UPS00233240](https://openairdocs.org/sdr/UPS00233240.md): Battery Pack · inoperative · Jul 6, 2000 · N918UP · Boeing 72730C · Emergency Lighting
  > EMERGENCY LIGHT FWD ENTRY DOOR INOPERATIVE. R/R EMERGENCY LIGHT AND BATTERY PACK. OPS CHECKED GOOD. P/N 10-00067 -9 SN ON 1315 SN OFF 900
- [SDR UPS00232107](https://openairdocs.org/sdr/UPS00232107.md): Light · inoperative · Mar 29, 2000 · N918UP · Boeing 72730C · Emergency Lighting
  > EMERGENCY LIGHT AT MAIN ENTRANCE DOOR IS INOPRATIVE. R/R EXIT LIGHT BATTERY ALL OPS CHECKS GOOD
- [SDR UPS99231178](https://openairdocs.org/sdr/UPS99231178.md): Light · failed · Dec 7, 1999 · N918UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:N/A, REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY (P/N 10-0067-7) (S/N 20261) OFF, REF IPC 33-50-00-20-15. REMOVED EMERGENCY EXIT LIGHT ASSY, OPS CHECK GOOD.
- [SDR UPS99231181](https://openairdocs.org/sdr/UPS99231181.md): Light · inop · Dec 6, 1999 · N918UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:N/A, BORROWED PART INSTALLED IN EMERGENCY EXIT LIGHT L1 POSITION. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IN L1 POSITION (P/N 10-0067-9) ON, (P/N 10- 0067-7) OFF, (S/N 2151) ON, (S/N 20261) OFF.
- [SDR UPS99229619](https://openairdocs.org/sdr/UPS99229619.md): Battery Pack · discharged · May 17, 1999 · N918UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:N/A, COCKPIT EMERGENCY LIGHTS ABOVE DOOR INOP, FAILED TO TEST. REMOVED UNIT FROM A/C, PUT BATTERIES ON CHARGE, REINSTALLED BATTS IN A/C AND OPS OK.
- [SDR UPS98227171](https://openairdocs.org/sdr/UPS98227171.md): Light · inoperative · Jul 15, 1998 · N918UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE-N/A, EMER EXIT LIGHT OVER FLIGHT DECK DOOR WILL NOT STAY IN IT'S ELECTRICAL SOCKET CAUSING IT TO STAY ON IN FLIGHT. REINSTALLED EMER EXIT LIGHT PROPERLY UNTILL LATCHES ENGAGED, EMER EXIT LIGHT, OPS CHECK GOOD.
- [SDR UPS98227164](https://openairdocs.org/sdr/UPS98227164.md): Batteries · discharged · Jul 14, 1998 · N918UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE-N/A, EMER EXIT LIGHT OVER FLIGHT DECK DOOR INOP. REPLACED WITH NEW BATTERIES, LIGHT OPS CHECKED OK.
- [SDR UPS97222408](https://openairdocs.org/sdr/UPS97222408.md): Light · inoperative · Mar 18, 1997 · N918UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHTS DO NOT TURN ON WITH SWITCH IN ON POSITION. REPLACED BATT ON EMERGENCY EXIT LIGHT, OPS CKS NORMAL.
- [SDR UPS97221862](https://openairdocs.org/sdr/UPS97221862.md): Light · inoperative · Jan 28, 1997 · N918UP · Boeing 72730C · Emergency Lighting
  > EMERGENCY EXIT LIGHT IN COCKPIT IS NOT SECURE AND CAME ON DURING LANDING ROLL OUT. RESECURED, OPS CHECKED GOOD.
- [SDR UPS97221835](https://openairdocs.org/sdr/UPS97221835.md): Shear Web · corroded · Jan 21, 1997 · N918UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, SHEAR WEB STA 1131 RBL 62 WL 208 HAS CORROSION AT NUTPLATE HOLE. CORROSION REMOVAL WAS OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED ALL WORK DONE IAW EO NR 727-53-1851 AND TRAMCO EWO 97-2020.
- [SDR UPS97221834](https://openairdocs.org/sdr/UPS97221834.md): Support Fitting · cracked · Jan 20, 1997 · N918UP · Boeing 72730C · Drag Control System
  > INSPECTION TYPE-C, NR 3 SPOILER SUPPORT FITTING ATTACH ANGLE IS CRACKED AT LOWER I/B ATTACH BOLT HOLE. REMOVED CRACKED NR 3 SPOILER SUPPORT FITTING ATTACH ANGLE. REPLACED PER SRM 51-30-2, MM 27-61-81, 27-61-0.
- [SDR UPS97221841](https://openairdocs.org/sdr/UPS97221841.md): Skin · cracked · Jan 15, 1997 · N918UP · Boeing 72730C · Trailing Edge Flaps
  > INSPECTION TYPE-C, LT WING I/B FOREFLAP L/E SKIN CRACKED FWD OF DEFLECTOR DOOR I/B END. REMOVED AND INSTALLED SERVICEABLE FOREFLAP, WORK DONE IAW MM 27-51-01.
- [SDR UPS97221833](https://openairdocs.org/sdr/UPS97221833.md): Angle · corroded · Jan 12, 1997 · N918UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C, CORROSION FOUND ON RT LOWER L-ANGLE RBL 24 BS 178 WL 207. FOUND CORROSION TO BE OUT OF LIMITS PER SRM 53-10-1. REPLACED L-ANGLE PER SRM 51-40-4, 53-10-2, 51-10-1, 51-10-6, 51-30-2.
- [SDR UPS97221840](https://openairdocs.org/sdr/UPS97221840.md): Hinge · corroded · Jan 11, 1997 · N918UP · Boeing 72730C · Leading Edge Devices
  > INSPECTION TYPE-C, NR 5 K-FLAP CENTER HINGE FITTING HAS SEVERAL SPOTS OF CORROSION. REMOVED AND INSTALLED NEW HINGE ASSY, WORK DONE IAW SRM 51-30-2, 51-30-5, 51-30-8, 51-10-2, 51-20-04, MM 27-87-01.

Next page: https://openairdocs.org/deregistered/N918UP-2007-11-21/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 = 'N918UP' AND deregistration_id = 'N918UP-2007-11-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N918UP-2007-11-21/reports

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